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Computational fluid dynamics
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The concept ** Computational fluid dynamics** represents the subject, aboutness, idea or notion of resources found in **University of Missouri-St. Louis Libraries**.

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Computational fluid dynamics
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**Computational fluid dynamics**represents the subject, aboutness, idea or notion of resources found in**University of Missouri-St. Louis Libraries**.- Label
- Computational fluid dynamics

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- [Analysis and development of finite element methods for the study of nonlinear thermomechanical behavior of structural components]
- 1998 NASA High-Speed Research Program Aerodynamic Performance Workshop : proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington D.C., and held in Los Angeles, California, February 9-13, 1998
- 1999 NASA High-Speed Research Program Aerodynamic Performance Workshop : proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington D.C., and held in Anaheim, California, February 8-12, 1999
- A CFD analysis of hydrogen leakage during on-pad purge in the ORION/ARES I shared volume
- A CFD study of tilt rotor flowfields
- A CFD-based study of the feasibility of adapting an erosion burner rig for examining the effect of CMAS deposition/corrosion on environmental barrier coatings
- A CFD/CSD interaction methodology for aircraft wings : a dissertation ...
- A comparison of interactional aerodynamics methods for a helicopter in low speed flight
- A comparison of lifting-line and CFD methods with flight test data from a research puma helicopter
- A computational examination of directional stability for smooth and chined forebodies at High-Ü
- A computational fluid dynamic and heat transfer model for gaseous core and gas cooled space power and propulsion reactors
- A computational investigation of gear windage
- A computational methodology for simulating thermal loss testing of the Advanced Stirling C
- A computational study of multiple jet and wall interaction
- A cost-effective strategy for nonoscillatory convection without clipping
- A critical comparison of turbulence models for homogeneous shear flows in a rotating frame
- A dual potential formulation of the Navier-Stokes equations
- A dual-plane PIV study of turbulent heat transfer flows
- A fast parallel tridiagonal algorithm for a class of CFD applications
- A generalized fluid system simulation program to model flow distribution in fluid networks : draft paper ...
- A generalized wall function
- A genuinely multi-dimensional upwind cell-vertex scheme for the Euler equations
- A high order discontinuous Galerkin method for 2D incompressible flows
- A high-order Lagrangian-decoupling method for the incompressible Navier-Stokes equations
- A high-order Lagrangian-decoupling method for the incompressible Navier-Stokes equations
- A hybrid numerical method for turbulent mixing layers
- A knowledge-based approach to automated flow-field zoning for computational fluid dynamics
- A least-squares finite element method for electromagnetic scattering problems
- A method for generating reduced order linear models of supersonic inlets : under grant NAG3-1450
- A method for generating reduced-order linear models of multidimensional supersonic inlets
- A modeling technique for STOVL ejector and volume dynamics
- A non-cut cell immersed boundary method for use in icing simulations
- A novel potential viscous flow coupling technique for computing helicopter flow fields
- A novel shape parameterization approach
- A numerical analysis of heat transfer and effectiveness on film cooled turbine blade tip models
- A numerical and experimental analysis of reactor performance and deposition rates for CVD on monofilaments
- A numerical method for incompressible flow with heat transfer
- A numerical turbulence model for multiphase flows in the protoplanetary nebula
- A preconditioning method for shape optimization governed by the Euler equations
- A robust design methodology for optimal microscale secondary flow control in compact inlet diffusers
- A sectored-one-dimensional model for simulating combustion instabilities in premix combustors
- A semantic analysis method for scientific and engineering code
- A simplified self-adaptive grid method, SAGE
- A study of pump cavitation damage
- A three-dimensional CFD investigation of secondary flow in an accelerating, 90 eÌŠlbow
- A three-dimensional unsteady CFD model of compressor stability
- A user's guide to CGNS
- A user's manual for ROTTILT solver : tiltrotor fountain flow field prediction
- ADPAC v1.0 : user's manual
- Accuracy of schemes for the Euler equations with no-nuniform meshes
- Accuracy of schemes with nonuniform meshes for compressible fluid flows
- Acoustical and flowfield characterization of a scaled tabletop rocket
- Acoustical and flowfield characterization of a scaled tabletop rocket
- Active control of flow separation over an airfoil
- Adaptive meshing techniques for viscous flow calculations on mixed element unstructured meshes
- Advanced low-noise research fan stage design
- Advanced space propulsion system flowfield modeling : final report : contract NAS8-40845
- Advanced space propulsion system flowfield modeling : final report : contract NAS8-40845
- Aero-heating of shallow cavities in hypersonic freestream flow
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ÌŠswept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
- Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations
- Aerodynamic design and computational analysis of a spacecraft cabin ventilation fan
- Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation
- Aerodynamic flow field measurements for automotive systems
- Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade
- Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade
- Aerodynamic performance of a compact, high work-factor centrifugal compressor at the stage and subcomponent level
- Aerodynamic synthesis of a centrifugal impeller using CFD and measurements
- Aerodynamic synthesis of a centrifugal impeller using CFD and measurements
- Aeroelastic analysis of aircraft : wing and wing/fuselage configurations
- Aeroelastic calculations using CFD for a typical business jet model
- Aeroelastic computations of a compressor stage using the harmonic balance method
- Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications : final report for the period December 1, 1995 through Novemeber 30, 1996
- Aeromechanics analysis of a boundary layer ingesting fan
- Aeropropulsion technology (APT) : task 23--stator seal cavity flow investigation
- Algebraic turbulence modeling for unstructured and adaptive meshes
- An LU implicit scheme for high speed inlet analysis
- An NPARC turbulence module with wall functions : under cooperative agreement NCC3-370
- An adaptive flow solver for air-borne vehicles undergoing time-dependent motions/deformations : annual technical progress report, period--August 1, 1996 - July 31, 1997, NASA grant no.--NAG-1-1760
- An application of the difference potentials method to solving external problems in CFD
- An application of the difference potentials method to solving external problems in CFD
- An automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization
- An efficient multiblock method for aerodynamic analysis and design on distributed memory systems : to be presented at the AIAA 13th Computational Fluid Dynamics Conference, June 1997
- An experimental and numerical investigation of turbulent vortex breakdown and aircraft wakes : final report, contract NAG 1-1775
- An experimental and numerical study of icing effects on the performance and controllability of a twin engine aircraft
- An experimental approach to a rapid propulsion and aeronautics concepts testbed
- An experimental investigation of a wing-fuselage junction model in the NASA Langley 14- by 22-foot subsonic tunnel
- An experimental study of the Ground Transportation System (GTS) model in the NASA Ames 7-by-10-Ft Wind Tunnel
- An incremental strategy for calculating consistent discrete CFD sensitivity derivatives
- An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients : semiannual progress report, July 1, 1987-December 31, 1987
- An inviscid computational study of an X-33 configuration at hypersonic speeds
- An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
- An upwind-differencing scheme for the incompressible Navier-Stokes equations
- Analysis of a hovering rotor in icing conditions
- Analysis of a rocket based combined cycle engine during rocket only operation
- Analysis of buzz in a supersonic inlet
- Analysis of coupled seals, secondary and powerstream flow fields in aircraft and aerospace turbomachines
- Analysis of inlet-compressor acoustic interactions using coupled CFD codes
- Analysis of inlet-compressor acoustic interactions using coupled CFD codes
- Analysis of internal flows relative to the space shuttle main engine : final report
- Analysis of lean premixed/prevaporized combustion with KIVA-II
- Analysis of low-speed stall aerodynamics of a swept wing with laminar-flow glove
- Analysis of the STS-126 flow control valve structural-acoustic coupling failure
- Analytical study of the origin and behavior of asymmetric vortices
- Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques
- Application of a Runge-Kutta scheme for high-speed inviscid internal flows
- Application of a high-fidelity icing analysis method to a model-scale rotor in forward flight
- Application of computational fluid dynamics in high speed aeropropulsion
- Application of low dimensional manifolds in NOx prediction : under cooperative agreement NCC3-534
- Applications of the Lattice Boltzmann method to complex and turbulent flows
- Ares I Scale Model Acoustic Test overpressure results
- Artificial boundary conditions based on the difference potentials method
- Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods
- Assessment of NASA's aircraft noise prediction capability
- Assessment of an explicit algebraic Reynolds stress model
- Assessment of computational fluid dynamics (CFD) models for shock boundary-layer interaction
- Assessment of some atomization models used in spray calculations
- Asynchronous communication of TLNS3DMB boundary exchange
- Atomization simulations using an Eulerian-VOF-Lagrangian method
- Automated boundary conditions for wind tunnel simulations
- Axial and centrifugal compressor mean line flow analysis method
- Axial-flow turbine rotor discharge-flow overexpansion and limit-loading condition, part 1, Computational fluid dynamics (CFD) investigation
- Axisymmetric calculations of a low-boom inlet in a supersonic wind tunnel
- Beta testing of CFD code for the analysis of combustion systems
- Bidirectional brush seals : post-test analysis
- Bidirectional brush seals--post-test analysis
- Blended wing body concept development with open rotor engine integration
- Burner rig with an unattached duct for evaluating the erosion resistance of thermal barrier coatings
- CFD analysis and design optimization using parallel computers
- CFD analysis of flexible thermal protection system shear configuration testing in the LCAT facility
- CFD analysis of nozzle jet plume effects on sonic boom signature
- CFD for hypersonic propulsion
- CFD modeling of free-piston Stirling engines
- CFD modelling of bore erosion in two-stage light gas guns
- CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report
- CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system : final report : under contract NAG3-1500
- CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction
- CFL3D contribution to the AIAA Supersonic Shock Boundary Layer Interaction Workshop
- CFL3D user's manual (version 5.0)
- CFL3D, its history and some recent applications
- CMOTT turbulence module for NPARC : under cooperative agreement NCC3-520
- Calculation of multistage turbomachinery using steady characteristic boundary conditions
- Calculation of turbulence-driven secondary motion in ducts with arbitrary cross section
- Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment
- Calculations of diffuser flows with an anisotropic K-[epsilon] model
- Capillary channel flow (CCF) EU2-02 on the International Space Station (ISS) : an experimental investigation of passive bubble separations in an open capillary channel
- Cause and cure : deterioration in accuracy of CFD simulations with use of high-aspect-ratio triangular/tetrahedral grids
- Combined experimental and numerical simulations of thermal barrier coated turbine blades erosion
- Comments on the diffusive behavior of two upwind schemes
- Comments on the diffusive behavior of two upwind schemes
- Comparative results from a CFD challenge over a 2D three-element high-lift airfoil
- Comparative study of advanced turbulence models for turbomachinery : contract NAS8-38860, final report
- Comparing spray characteristics from Reynolds Averaged Navier-Stokes (RANS) National Combustion Code (NCC) calculations against experimental data for a turbulent reacting flow
- Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental data
- Comparison of NACA 0012 laminar flow solutions : structured and unstructured grid methods
- Comparison of high-order and low-order methods for large-eddy simulation of a compressible shear layer
- Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine
- Comparison of several numerical methods for simulation of compressible shear layers
- Comparison of the booster interface temperature in stainless steel (SS) v-channel versus the aluminum (Al) y-channel Primer Chamber Assemblies (PCAs)
- Comparison of theoretical and flight-measured local flow aerodynamics for a low-aspect-ratio fin
- Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
- Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating
- Compliant turbomachine sealing
- Compressibility considerations for [kappa-omega] turbulence models in hypersonic boundary layer applications
- Compressible flows with periodic vortical disturbances around lifting airfoils
- Computation of Navier-Stokes equations for three-dimensional flow separation
- Computation of lifting wing-flap configurations : NASA grant NCC2-5070, final report ... funding dates: July 1, 1994 to June 30, 1995
- Computation of potential flows with embedded vortex rings and applications to helicopter rotor wakes
- Computation of separated and unsteady flows with one- and two-equation turbulence models : 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994/Reno, NV
- Computation of sound generated by viscous flow over a circular cylinder
- Computation of sound generated by viscous flow over a circular cylinder
- Computation of viscous flow in curved ducts and comparison with experimental data
- Computation of viscous incompressible flows
- Computational Fluid Dynamics (CFD) analysis for the reduction of impeller discharge flow distortion
- Computational Fluid Dynamics (CFD) simulations of jet mixing in tanks of different scales
- Computational aeroacoustics and numerical simulation of supersonic jets : final report on NASA grant NAG 1-1479
- Computational aerodynamic simulations of a 1484 ft/sec tip speed quiet high-speed fan system model for acoustic methods assessment and development
- Computational aerodynamic simulations of a spacecraft cabin ventilation fan design
- Computational aerodynamic simulations of an 840 ft/sec tip speed advanced ducted propulsor fan system model for acoustic methods assessment and development
- Computational aeroheating predictions for X-34
- Computational aeroheating predictions for X-34
- Computational aeroservoelastic analysis with an Euler-based unsteady flow solver : NASA-Ames university consortium cooperative agreement no. NCC2-5105, final research summary for the period: 1 November 1994 - 31 January 1997
- Computational analyses of propulsion aeroacoustics for mixed flow nozzle pylon installation at takeoff
- Computational analysis of a low-boom supersonic inlet
- Computational analysis of the SSME fuel preburner flow : final report
- Computational analysis of the combustion process in an axisymmetric RBCC flowpath
- Computational analysis of the combustion process in an axisymmetric,RBCC flowpath
- Computational assessment of the aerodynamic performance of a variable-speed power turbine for large civil tilt-rotor application
- Computational fluid mechanics utilizing the variational principle of modeling damping seals
- Computational icing risk analysis of the D8 "Double Bubble" aircraft
- Computational investigation of flap-edges : final report, NASA award NCC-2-857
- Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades
- Computational investigation of tangential slot blowing on a generic chined forebody
- Computational modeling and validation for hypersonic inlets
- Computational pollutant environment assessment from propulsion-system testing
- Computational simulations of convergent nozzles for the AIAA 1st Propulsion Aerodynamics Workshop
- Computational study of near-limit propagation of detonation in hydrogen-air mixtures
- Computational study of near-limit propagation of detonation in hydrogen-air mixtures
- Computational study of separating flow in a planar subsonic diffuser
- Computational study of surface tension and wall adhesion effects on an oil film flow underneath an air boundary layer
- Computational study of the CC3 impeller and vaneless diffuser experiment
- Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations
- Computational test cases for a rectangular supercritical wing undergoing pitching oscillations
- Computational work to support FAP/SRW variable-speed power-turbine development
- Computational/experimental aeroheating predictions for X-33 phase II vehicle
- Computations of axisymmetric flows in hypersonic shock tubes
- Computations of complex three-dimensional turbulent free jets
- Computer Aided Grid Interface : an interactive CFD pre-processor, final report, (performance period--16 May 1991-15 May 1996)
- Computer simulation of aircraft aerodynamics
- Concept evaluation : NASA reference model 2--side by side
- Conjugate heat transfer analyses on the manifold for ramjet fuel injectors
- Connection between the lattice Boltzmann equation and the beam scheme
- Conservational PDF equations of turbulence
- Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computers
- Convergence acceleration of a Navier-Stokes solver for efficient static aeroelastic computations
- Convergence analysis of turbulent flow solutions
- Correlation of Puma airloads : lifting-line and wake calculation
- Correlation of puma airloads : evaluation of CFD prediction methods
- Critical assessment of Reynolds stress turbulence models using homogeneous flows
- Cryogenic fluid storage technology development : recent and planned efforts at NASA
- Current capabilities and future directions in computational fluid dynamics
- Current status of post-combustor trace chemistry modeling and simulation at NASA Glenn Research Center
- Current status of superheat spray modeling with NCC
- Data Parallel Line Relaxation (DPLR) code user manual : Acadia version 4.01.1
- Data driven model development for the supersonic semispan transport (S4T)
- Design and analysis of an isokinetic sampling probe for submicron particle measurements at high altitude
- Design and analysis tool for external-compression supersonic inlets
- Detailed experimental data for CFD code validation
- Deterministic stress modeling of hot gas segregation in a turbine
- Development and demonstration of a computational tool for the analysis of particle vitiation effects in hypersonic propulsion test facilities
- Development and life prediction of erosion resistant turbine low conductivity thermal barrier coatings
- Development and validation of a multidisciplinary tool for accurate and efficient rotorcraft noise prediction (MUTE)
- Development and validation of a supersonic helium-air coannular jet facility
- Development of a computational aero/fluids analysis system : final report
- Development of a fluid structures interaction test technique for fabrics
- Development of a grid-independent approximate Riemann solver
- Development of an automatic differentiation version of the FPX rotor code
- Development of an axisymmetric afterbody test case for turbulent flow separation validation
- Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations : final technical report
- Development of detonation modeling capabilities for rocket test facilities : hydrogen-oxygen-nitrogen mixtures
- Development of improved surface integral methods for jet aeroacoustic predictions : final report, NASA-Langley grant no. NAG-1660
- Development of the Glenn Heat-Transfer (Glenn-HT) computer code to enable Time-Filtered Navier-Stokes (TFNS) simulations and application to film cooling on a flat plate through long cooling tubes
- Development of three-dimensional DRAGON grid technology
- Development of three-dimensional DRAGON grid technology
- Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination
- Development of tripropellant CFD design code : contract no.--NAS8-40583 : final report
- Development, verification and use of gust modeling in the NASA computational fluid dynamics code FUN3D
- Direct numerical simulation of a temporally evolving incompressible plane wake : effect of initial conditions on evolution and topology
- Direct numerical simulation of incompressible pipe flow using a B-spline spectral method
- Direct numerical simulation of incompressible pipe flow using a b-spline spectral method
- Drag reduction on circular cylinders by ejecting jet from rear stagnation region : progress report for the period ending June 30, 1997 ... under Cooperative Agreement NCC1-232
- Dual-pump CARS development and application to supersonic combustion
- Duct flow nonuniformities : effects of struts in SSME HGM II+ : interim report
- Duct flow nonuniformities study for Space Shuttle main engine : technical report
- Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach
- Dynamic stall suppression using combustion-powered actuation (COMPACT)
- Dynamical approach study of spurious steady-state numerical solutions of nonlinear differential equations
- Dynamics of large-scale structures for jets in crossflow
- Dynamics of superfluid helium in low-gravity : NASW-4803, final report
- Effect of coannular flow on linearized Euler equation predictions of jet noise
- Effect of curvature on the impact damage characteristics and residual strength of composite plates
- Effect of turbulence modeling on an excited jet
- Effect of turbulence models on two massively-separated benchmark flow cases
- Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads
- Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan
- Effects of rotation on coolant passage heat transfer
- Efficient gradient-based shape optimization methodology using inviscid/viscous CFD : summary of research report for the period of March 9, 1995 to March 8, 1997, grant# NCC-1-211
- Efficient grid generation : final report
- Efficient parallel kernel solvers for computational fluid dynamics applications : final report, NASA contract no. NAG1-1672 (Jan. 1995-Aug. 97)
- Energy efficient engine low pressure subsystem flow analysis
- Energy transfer and triadic interactions in compressible turbulence : under contract NAS1-19480
- Engineering aerothermal analysis for X-34 thermal protection system design : 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV
- Enhanced design of turbo-jet LPT by separation control using phased plasma actuators
- Enhanced multiobjective optimization technique for comprehensive aerospace design : final report on NCC2-5150
- Enhancing aeropropulsion research with high-speed interactive computing
- Entropy splitting and numerical dissipation
- Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing
- Essential elements of computational algorithms for aerodynamic analysis and design : under contracts NAS1-97046 & NAS1-19480
- Euler flow computations on non-matching unstructured meshes
- Euler technology assessment : SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts
- Euler technology assessment for preliminary aircraft design : unstructured/structured grid NASTD application for aerodynamic analysis of an advanced fighter/tailless configuration
- Euler/Navier-Stokes flow computations on flexible configurations for stability analysis
- Evaluation of CFD turbulent heating prediction techniques and comparison with hypersonic experimental data
- Evaluation of an adaptive unstructured remeshing technique for integrated fluid-thermal-structural analysis
- Evaluation of inflow turbulence methods in large-eddy simulations of a supersonic boundary layer
- Evaluation of turbulence models for unsteady flows of an oscillating airfoil
- Examination of wave speed in rotating detonation engines using simplified computational fluid dynamics : prepared for 2018 SciTech Forum spnsored by the American Institute of Aeronautics and Astronautics Kissimmee, Florida, January 8-12, 2018
- Exhaust nozzle plume and shock wave interaction
- Exhaust nozzle plume effects on sonic boom test results for isolated nozzles
- Exhaust nozzle plume effects on sonic boom test results for vectored nozzles
- Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft
- Experimental and computational aerothermodynamics of a Mars entry vehicle
- Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle
- Experimental and computational sonic boom assessment of Boeing N+2 low boom models
- Experimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models
- Experimental database with baseline CFD solutions : 2-D and axisymmetric hypersonic shock-wave/turbulent-boundary-layer interactions
- Experimental evaluation of the effect of angle-of-attack on the external aerodynamics and mass capture of a symmetric three-engine air-breathing launch vehicle configuration at supersonic speeds
- Experimental investigation of Mars Science Laboratory entry vehicle aeroheating in AEDC hypervelocity tunnel 9
- Experimental investigation of hexcomb-pattern roughness effects on transition onset and turbulent heating augmentation at Mach 6
- Experimental program for real gas flow code validation at NASA Ames Research Center
- Exploring a method for improving turbulent separated-flow predictions with [k-omega] models
- Extension of a kinetic approach to chemical reactions to electronic energy levels and reactions involving charged species with application to DSMC simulations
- Extension of a streamwise upwind algorithm to a moving grid system
- Extension of a three-dimensional viscous wing flow analysis
- Extension of a three-dimensional viscous wing flow analysis : user's manual : VISTA 3-D code
- Extension of an object-oriented optimization tool : use's reference manual
- Extension of transonic flow computational concepts in the analysis of cavitated bearings
- External boundary conditions for three-dimensional problems of computational aerodynamics
- F-16XL-2 supersonic laminar flow control flight test experiment
- FUN3D manual : 13.6
- FUN3D manual, 12.5
- Fan noise source diagnostic test computation of rotor wake turbulence noise
- Fan noise source diagnostic test computation of rotor wake turbulence noise
- Final report for parallel computation of unsteady flows on a network of workstations (NAG3-1577) for the period of 1993-1997
- Final report for the shuttle flight experiment on USMP-4 : in situ monitoring of crystal growth using MEPHISTO
- First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop : proceedings of a workshop held at Langley Research Center, Hampton, Virginia, February 27-29, 1996
- Flamelet model application for non-premixed turbulent combustion : final report under cooperative agreement no. NCCW-75 ...
- Flat plate wake velocity statistics obtained with circular and elliptic trailing edges
- Flight test results on the stability and control of the F-15 Quiet Spike aircraft
- Flight testing the linear aerospike SR-71 experiment (LASRE)
- Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
- Flow analysis of the Cleveland clinic centrifugal pump
- Flow analysis of the Cleveland clinic centrifugal pump
- Flow control under low-pressure turbine conditions using pulsed jets : final report
- Flow distribution around the SSME main injector assembly using porosity formulation
- Flow field characterization of an angled supersonic jet near a bluff body
- Flowfield computation of entry vehicles
- Flowfield-dependent mixed explicit-implicit (FDMEI) algorithm for computational fluid dynamics : final report ...
- Fluid acquisition and resupply experiments on space shuttle flights STS-53 and STS-57
- Flutter sensitivity to boundary layer thickness, structural damping, and static pressure differential for a shuttle tile overlay repair concept
- Forced mixer nozzle optimization
- Free-form airfoil shape optimization under uncertainty using maximum expected value and second-order second-moment strategies
- Fuel flexible combustor for high-OPR compact-core N+3 propulsion engine : final technical report
- Fuel injector design optimization for an annular scramjet geometry
- Fundamental ice crystal accretion physics studies
- Fundamental study of a single point lean direct injector part I : effect of air swirler angle and injector tip location on spray characteristics
- Funding and strategic alignment guidance for infusing small business innovation research technology into NASA programs associated with the Human Exploration and Operations Mission Directorate
- Further development of a method for computing three-dimensional subsonic viscous flows in turbofan lobe mixers
- Further validation of a CFD code for calculating the performance of two-stage light gas guns
- GRID2D/3D, a computer program for generating grid systems in complex-shaped two- and three-dimensional spatial domains
- Generation of performance model for the Aeolian Wind Tunnel (AWT) rotor at reduced pressure
- Geometry and simulation results for a gas turbine representative of the energy efficient engine (EEE)
- Global artificial boundary conditions for computation of external flow problems with propulsive jets
- Globalized Newton-Krylov-Schwarz algorithms and software for parallel implicit CFD
- Growth characteristics downstream of a shallow bump : computation and experiment
- Heat transfer computations of internal duct flows with combined hydraulic and thermal developing length
- Heat transfer on a film-cooled rotating blade
- Helicopter blade-vortex interaction noise with comparisons to CFD calculations
- Helicopter blade-vortex interaction noise with comparisons to CFD calculations
- Helicopter rotor blade computation in unsteady flows using moving overset grids
- Hierarchical and parallelizable direct volume rendering for irregular and multiple grids
- High fidelity CFD analysis and validation of rotorcraft gearbox aerodynamics under operational and oil-out conditions : final report
- High order finite difference and finite volume WENO schemes and discontinuous Galerkin methods for CFD
- High resolution Euler solvers based on the space-time conservation element and solution element method
- High-order space-time methods for conservation laws
- Higher-order compact schemes for numerical simulation of incompressible flows
- Hopf bifurcation in the driven cavity
- Hydrodynamic design of the fastrac turbopump
- Hypersonic pitching-moment shift for stardust reentry capsule forebody
- ICEG2D--an integrated software package for automated prediction of flow fields for single-element airfoils with ice accretion
- Ice crystal icing research at NASA
- Ice-accretion test results for three large-scale swept-wing models in the NASA Icing Research Tunnel
- Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques
- Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques
- Impact of an exhaust throat on semi-idealized rotating detonation engine performance
- Impact of load balancing on unstructured adaptive grid computations for distributed-memory multiprocessors
- Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines
- Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade
- Implementation of advanced two equation turbulence models in the USM3D unstructured flow solver
- Improvements to an explicit algebraic stress model for turbulent jet mixing predictions
- Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance
- Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ÌŠangle of attack : contract NAS 3-26617
- Inspection of the Math Model Tools for on-orbit assessment of impact damage report
- Interaction of sound from supersonic jets with nearby structures
- Interactive algebraic grid-generation technique
- Internal passage heat transfer prediction using multiblock grids and a [kappa-omega] turbulence model : under cooperative agreement NCC3-370
- Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
- Investigation of active flow control to improve aerodynamic performance of oscillating wings
- Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems : final report, Task 1, Ducted propfan analysis
- Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
- Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
- Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms
- Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
- Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
- Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24
- Isolated rotor forward flight testing at Martian atmospheric density data report
- Jet noise physics and modeling using first-principles simulations
- Jet noise reduction potential from emerging variable cycle technologies
- LES of a jet excited by the Localized Arc Filament Plasma Actuators
- LES, DNS, and RANS for the analysis of high-speed turbulent reacting flows : annual report submitted to NASA Langley Research Center : progress report ... under grant NAG 1-1122 for the period August 1, 1995 - July 31, 1996
- LSPRAY : a Lagrangian spray solver, user's manual : prepared under contract NAS3-27186
- LSPRAY-IV : a lagrangian spray module
- LTCP 2D graphical user interface : application description and user's guide
- Lagrangian approach to jet mixing and optimization of the reactor for production of carbon nanotubes
- Large eddy simulation of transonic flow field in NASA rotor 37
- Large-scale parallel viscous flow computations using an unstructured multigrid algorithm
- Laser anemometer measurements of the flow field in a 4:1 pressure ratio centrifugal impeller
- Laser anemometer measurements of the flow field in a 4:1 pressure ratio centrifugal impeller
- Lecture series in computational fluid dynamics
- Linear instability of a uni-directional transversely sheared mean flow
- Long hole film cooling dataset for CFD development, Part 1, Infrared thermography and thermocouple surveys
- Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds
- Low-Reynolds number aerodynamics of an 8.9 percent scale semispan swept wing for assessment of icing effects
- Mach 10 experimental database of a three-dimensional scramjet inlet flow field
- Mach 5 inlet CFD and experimental results
- Magnetically actuated propellant orientation experiment, controlling fluid motion with magnetic fields in a low-gravity environment : (MSFC Center Director's Discretionary Fund final report, project no. 93-18)
- Mars entry atmospheric data system modeling, calibration, and error analysis
- Mars sample return : Mars Ascent Vehicle mission & technology requirements
- Mass transfer from a sphere in an oscillating flow with zero mean velocity
- Mean velocity and turbulence measurements in a 90Â° curved duct with thin inlet boundary layer : final report
- Measuring global surface pressures on a circulation control concept using pressure sensitive paint
- Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications : final report for the period ended December 31, 1995
- Methods for computationally efficient structured CFD simulations of complex turbomachinery flows
- Micro-ramp flow control for oblique shock interactions : comparisons of computational and experimental data
- Mid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept
- Mir cooperative solar array flight performance data and computational analysis
- Mixing enhancement by tabs in round supersonic jets
- Modeling of turbulent swirling flows
- Modeling of unsteady three-dimensional flows in multistage machines
- Modeling the dissipation rate in rotating turbulent flows
- Modeling vortex generators in the Wind-US Code
- Modelling the transitional boundary layer
- Multigrid method for stability problems
- Multiphysics simulation of active hypersonic lip cooling
- Multiprocessing on supercomputers for computational aerodynamics
- NASA N+2 advanced low NOx combustor technology
- NASA Rotor 37 CFD code validation : Glenn-HT code
- NASA numerical and experimental evaluation of UTRC low emissions injector
- NASA one-dimensional combustor simulation : user manual for S1D_ML
- NPSS multidisciplinary integration and analysis
- National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program - 1995 : grant NGT 44-001-800
- National combustion code parallel performance enhancements
- Navier-Stokes analysis of the flowfield characteristics of an ice contaminated aircraft wing
- Navier-Stokes computations on full wing-body configuration with oscillating control surfaces
- Navier-Stokes simulation of several high-lift reference H configurations
- Navier-Stokes simulation of the crossflow instability in swept-wing flows : a final report to National Aeronautics and Space Administration, Langley Research Center ; submitted by Helen L. Reed
- Near-wall, three-dimensional turbulence measurements : a challenge for laser velocimetry
- Nearly interactive Parabolized Navier-Stokes solver for high speed forebody and inlet flows
- New computational methods for the prediction and analysis of helicopter noise
- Ninth Thermal and Fluids Analysis Workshop proceedings : proceedings of a conference held at ... NASA Glenn Research Center, Cleveland, Ohio, August 31-September 4, 1998
- Nonlinear axisymmetric and three-dimensional vorticity dynamics in a swirling jet model
- Nonlinear dynamics & numerical uncertainties in CFD
- Nozzle plume/shock interaction experimental and computational sonic boom analyses from the NASA Ames 9-by 7-foot supersonic wind tunnel
- Numerical analysis of a rotating detonation engine in the relative reference frame
- Numerical analysis of base flowfield for a four-engine clustered nozzle configuration
- Numerical assessment of four-part through-flow wave rotor cycles with passage height variation
- Numerical assessment of four-port through-flow wave rotor cycles with passage height variation
- Numerical flow visualization in basic- and hyper-cluster spheres
- Numerical flow visualization in basic- and hyper-cluster spheres
- Numerical modeling of spray combustion with an advanced VOF method
- Numerical simulation methods of incompressible flows and an application to the space shuttle main engine
- Numerical simulation of a low emissions gas turbine combustor using KIVA-II, Part I, Fuel nozzle/rich-burn zone analysis
- Numerical simulation of a low emissions gas turbine combustor using KIVA-II, Part II, Quick-quench/lean-combustion zones analysis
- Numerical simulation of complex turbomachinery flows
- Numerical simulation of high-speed turbulent reacting flows : annual report submitted to the NASA Langley Research Center, progress report on activities supported under grant NAG 1-1122 for the period August 1, 1996 - July 31, 1997
- Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D
- Numerical simulation of low-density shock-wave interactions
- Numerical simulation of scramjet inlet flow fields
- Numerical simulation of vitiation effects on a hydrogen-fueled dual-mode scramjet
- Numerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design
- Numerical simulations of two-phase reacting flow in a single-element lean direct injection (LDI) combustor using NCC
- Numerical solutions of the complete Navier-Stokes equations : final report : NASA grant NAG-1-244
- Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models
- Numerical study of stratified charge combustion in wave rotors
- Numerical study of stratified charge combustion in wave rotors
- Numerically simulating an expanding continuum jet into a surrounding non-continuum region
- Object-oriented implementation of the NAS parallel benchmarks using charm++ : annual report
- Observations on computational methodologies for use in large-scale, gradient-based, multidisciplinary design incorporating advanced CFD codes
- Observations regarding use of advanced CFD analysis, sensitivity analysis, and design codes in MDO
- On applications of Chimera grid schemes to store separation
- On approximate factorization schemes for solving the full potential equation
- On approximate factorization schemes for solving the full potential equation
- On convergence acceleration techniques for unstructured meshes
- On formulations of discontinuous Galerkin and related methods for conservation laws
- On multifunctional collaborative methods in engineering science
- On the coupling of CDISC design method with FPX rotor code
- Optical characterization of a multipoint lean direct injector for gas turbine combustors : velocity and fuel drop size measurements
- Optimization of an advanced design three-element airfoil at high Reynolds numbers
- Orion Service Module Reaction Control System plume impingement analysis using PLIMP/RAMP2
- Overview of ICE project : integration of computational fluid dynamics and experiments
- Overview of ICE project : integration of computational fluid dynamics and experiments
- Overview of heat addition and efficiency predictions for an advanced stirling convertor
- Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project
- PIV and rotational Raman-based temperature measures for CFD validation in a single injector cooling flow
- PLOT3D user's manual
- PLTTER user's guide
- Parallel ALLSPD-3D : speeding up combustor analysis via parallel processing
- Parallel ALLSPD-3D : speeding up combustor analysis via parallel processing
- Parallel Newton-Krylov-Schwarz algorithms for the transonic full potential equation : NASA contract no. NAS1-19480
- Parallel implementation of an adaptive scheme for 3D unstructured grids on the SP2
- Parallelization of the implicit RPLUS algorithm : final report, NASA grant NAG 3-1472
- Parallelizing Navier-Stokes computations on a variety of architectural platforms
- Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system
- Parametric study of decay of homogeneous isotropic turbulence using large eddy simulation
- Particle kinetic simulation of high altitude hypervelocity flight : periodic research report for the period February 1, 1992 - December 31, 1992
- Passive rocket diffuser testing : reacting flow performance of four second-throat geometries
- Passive rocket diffuser theory : a re-examination of minimum second throat size
- Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations
- Performance evaluation of the NASA GTX RBCC flowpath
- Performance gains of propellant management devices for liquid hydrogen depots
- Performance impact of deflagration to detonation transition enhancing obstacles
- Performance improvement through indexing of turbine airfoils, Part 2, Numerical simulation
- Performance of the widely-used CFD code OVERFLOW on the Pleides supercomputer
- Physics of forced unsteady separation : proceedings of a NASA/AFOSR/ARO workshop held at NASA Ames Research Center, Moffett Field, California, April 17-19, 1990
- Planar Inlet Design and Analysis Process (PINDAP)
- Potential application of NASA aerospace technology to ground-based power systems
- Potential application of NASA aerospace technology to ground-based power systems
- Preconditioning for numerical simulation of low Mach number three-dimensional viscous turbomachinery flows
- Preconditioning methods for low-speed flows
- Predicting modes of the unsteady vorticity field near the trailing edge of a blade
- Predicting turbulent convective heat transfer in three-dimensional duct flows
- Predicting turbulent convective heat transfer in three-dimensional duct flows
- Prediction of complex aerodynamic flows with explicit algebraic stress models : 34th Aerospace Sciences Meeting & Exhibit, January 15-18, 1996/Reno, NV
- Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn
- Prediction of relaminarization effects on turbine blade heat transfer
- Preliminary aerodynamic investigation of fan rotor blade morphing
- Preprocessor that enables the use of GridPro grids for unsteady Reynolds-averaged Navier-Stokes code TURBO
- Production level CFD code acceleration for hybrid many-core architectures
- Progress in grid generation : from chimera to DRAGON grids
- Progress in grid generation : from chimera to DRAGON grids
- Progress of high efficiency centrifugal compressor simulations using TURBO
- Prospects for CFD on petaflops systems
- Quiet, efficient fans for spaceflight : an overview of NASA's technology development plan
- RNS applications for interacting sub- and supersonic flows : final report, NASA grant no. NAG1-1553, 11/19/93-5/18/97
- Radiation-spray coupling for realistic flow configurations
- Rapid mix concepts for low emission combustors in gas turbine engines
- Rapid prediction of unsteady three-dimensional viscous flows in turbopump geometries : progress report 2
- Recalibration of the shear stress transport model to improve calculation of shock separated flows
- Recent development in the CESE method for the solution of the Navier-Stokes Equations using unstructured triangular or tetrahedral meshes with high aspect ratio
- Recent progress in research pertaining to estimates of gas-side heat transfer in an aircraft gas turbine
- Reduced Navier Stokes relaxation procedures for internal flows : final report, NASA grant no. NAG3-397, 3/01/83-2/28/96
- Reentry-F flowfield solutions at 80,000 ft
- Requirements for large eddy simulation computations of variable-speed power turbine flows
- Research in computational aeroscience applications implemented on advanced parallel computing systems : final report for first year of prime contract NAS2-14090
- Research in progress : applied and numerical mathematics : semiannual report, October 1, 1995 through March 31, 1996
- Research on supersonic inlet bleed
- Results of an advanced fan stage operating over a wide range of speed and bypass ratio
- Results of the integration of a transonic full-potential analysis program with a free-wake lifting-line program for hovering rotors
- Review of Godunov methods
- Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments
- Rocket-based combined cycle engine technology development : inlet CFD validation and application
- Rocket-based combined cycle engine technology development : inlet CFD validation and application
- Role of computational fluid dynamics and wind tunnels in aeronautics R&D
- RotCFD analysis of the AH-56 Cheyenne hub drag
- Rotor CFD analysis at terrestrial and martian atmospheric densities
- Rotor vortex filaments : living on the slipstream's edge
- Rotor vortex filaments : living on the slipstream's edge
- Rotorcraft application of advanced computational aerodynamics
- SAGE, the self-adaptive grid codE, version 3
- SRM internal flow test and computational fluid dynamic analyses : final report : contract NAS8-39095
- SSME LOX post flow analysis/fluid structure interaction : final report
- STARS, an integrated, multidisciplinary, finite-element, structural, fluids, aeroelastic, and aeroservoelastic analysis computer program
- STARS, an integrated, multidisciplinary, finite-element, structural, fluids, aeroelastic, and aeroservoelastic analysis computer program
- Scaling of data communications for an advanced supercomputer network
- Secondary frequencies in the wake of a circular cylinder with vortex shedding
- Self-recirculating casing treatment concept for enhanced compressor performance
- Seventh Copper Mountain Conference on Multigrid Methods
- Shock wave interaction with an abrupt area change
- Silent aircraft initiative concept risk assessment
- Simulation of VSPT experimental cascade under high and low free-stream turbulence conditions
- Simulation of a controlled airfoil with jets
- Simulation of glancing shock wave and boundary layer interaction
- Simulation of supersonic jet noise with the adaptation of overflow CFD code and Kirchhoff surface integral
- Simulation of supersonic jet noise with the adaptation of overflow CFD code and Kirchhoff surface integral
- Simulation of two-fluid flows by the least-squares finite element method using a continuous surface tension model
- Simulation of unsteady hypersonic combustion around projectiles in an expansion tube
- Simulations of spray reacting flows in a single element LDI injector with and without invoking an Eulerian scalar PDF method
- Simulations of the Mars helicopter test propeller in hover configuration at Martian pressure and air density
- Simulations of turbine cooling flows using a multiblock-multigrid scheme : under cooperative agreement NCC3-370
- Slot nozzle effects for reduced sonic boom on a generic supersonic wing section
- SmaggIce 2.0 : additional capabilities for interactive grid generation of iced airfoils
- SmaggIce : surface modeling and grid generation for iced airfoils, phase I results
- SmaggIce user guide : SmaggIce version 1.0
- SmaggIce, surface modeling and grid generation for iced airfoils : phase 1 results
- Small engine technology (set) Task 8, aeroelastic prediction methods : final report : prepared under contract NAS3-27483
- Small scale mass flow plug calibration
- Solar thermal upper stage liquid hydrogen pressure control testing