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

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Flow distribution
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The concept

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

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- nasat

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- Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes
- A CFD study of tilt rotor flowfields
- A closure for the compressibility of the source terms in lighthill's acoustic analogy
- A computational examination of directional stability for smooth and chined forebodies at High-Ü
- A critical survey of optimization models for tactical and strategic aspects of air traffic flow management
- A data base and analysis program for shuttle main engine dynamic pressure measurements : final report
- A generalized fluid system simulation program to model flow distribution in fluid networks : draft paper ...
- A knowledge-based approach to automated flow-field zoning for computational fluid dynamics
- A multi-domain spectral method for supersonic reactive flows
- A note on trapping moving vortices
- A novel potential viscous flow coupling technique for computing helicopter flow fields
- A numerical turbulence model for multiphase flows in the protoplanetary nebula
- A package for 3-D unstructured grid generation, finite-element flow solution and flow field visualization
- A parametric study of accelerations of an airplane due to a wake vortex system
- A parametric study of accelerations of an airplane due to a wake vortex system
- A planar reacting shear layer system for the study of fluid dynamics-combustion interaction
- A quiet tunnel investigation of hypersonic boundary-layer stability over a cooled, flared cone : final report
- A reduced order model of the linearized incompressible Navier-Strokes equations for the sensor/actuator placement problem
- A robust design methodology for optimal microscale secondary flow control in compact inlet diffusers
- A simplified model for detonation based pressure-gain combustors
- A smoke generator system for aerodynamic flight research
- A user's manual for ROTTILT solver : tiltrotor fountain flow field prediction
- A wall interference assessment/correction interface measurement system for the NASA-ARC 12-FT PWT : final memorandum report
- AST combustion workshop : diagnostic working group report
- Acoustical and flowfield characterization of a scaled tabletop rocket
- Acoustical and flowfield characterization of a scaled tabletop rocket
- Adaptive grid embedding for the two-dimensional flux-split Euler equations
- Advanced noise control fan aerodynamic performance
- Advanced space propulsion system flowfield modeling : final report : contract NAS8-40845
- Advanced space propulsion system flowfield modeling : final report : contract NAS8-40845
- Aerodynamic calibration of the NASA Lewis icing research tunnel (1997 tests)
- Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations
- Aerodynamic classification of swept-wing ice accretion
- Aerodynamic flow field measurements for automotive systems
- Aerodynamic performance of a compact, high work-factor centrifugal compressor at the stage and subcomponent level
- Aeropropulsion technology (APT) : task 23--stator seal cavity flow investigation
- Aerothermal tests of a 12.5Â° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes
- Air traffic management technology demonstration- 3 (ATD-3) multi-flight common route (MFCR) concept of operations : version 1.0
- Air-jet milling of grinding materials
- An LU implicit scheme for high speed inlet analysis
- An approximate method for calculating three-dimensional inviscid hypersonic flow fields
- An evaluation of measured pressure signatures from wind-tunnel models of three low-boom concepts
- An experimental investigation of a wing-fuselage junction model in the NASA Langley 14- by 22-foot subsonic tunnel
- An experimental investigation of steady and unsteady flow field in an axial flow turbine
- An experimental study of characteristic combustion-driven flow for CFD validation : final report for NASA contract NAS8-38862
- An experimental study of swirling flows as applied to annular combustors : a thesis ...
- An experimental study of the turbulent boundary layer on a transport wing in subsonic and transonic flow
- An investigation of candidate sensor-observable wake vortex strength parameters for the NASA Aircraft Vortex Spacing System (AVOSS) : under cooperative agreement NCC1-24
- An upwind-differencing scheme for the incompressible Navier-Stokes equations
- Analysis and design of optimized truncated scarfed nozzles subject to external flow effects
- Analysis of coupled seals, secondary and powerstream flow fields in aircraft and aerospace turbomachines
- Analysis of inviscid and viscous flows in cascades with an explicit multiple-grid algorithm
- Application of a self-adaptive grid method to complex flows
- Application of an efficient hybrid scheme for aeroelastic analysis of advanced propellers
- Application of computational fluid dynamics in high speed aeropropulsion
- Application of laser velocimetry to unsteady flows in large scale high speed tunnels
- Application of particle image velocimetry to a study of flow about a multi-element airfoil : final report for the period August 15, 1995 to August 14, 1996 ... grant no. NCC2-5155
- Approaches to validation of models for low gravity fluid behavior
- Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor
- Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor
- Autoclave processing for composite material fabrication. 1. An analysis of resin flows and fiber compactions for thin laminate.
- Automated fluid feature extraction from transient simulations : progress report
- Boundary layer flow control by an array of ramp-shaped vortex generators
- CFD for hypersonic propulsion
- CFD study of NACA 0018 airfoil with flow control
- CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system : final report : under contract NAG3-1500
- Calibration of NASA Lewis Research Center 9- by 15-Foot low speed wind tunnel (1992 text)
- Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel (1996 and 1997 tests)
- Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)
- Challenges to laser-based imaging techniques in gas turbine combustor systems for aerospace applications
- Challenges to laser-based imaging techniques in gas turbine combustor systems for aerospace applications
- Characterization of three-stream jet flow fields
- Coarse grid modeling of turbine film cooling flows using volumetric source terms
- Coarse grid modeling of turbine film cooling flows using volumetric source terms
- Comparison of the aeroacoustics of two small-scale supersonic inlets : final technical report, NASA contract #--NAG 3-1539
- Comparison of tomo-PIV versus dual plane PIV on a synthetic jet flow
- 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 separated and unsteady flows with one- and two-equation turbulence models : 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994/Reno, NV
- Computation of viscous flow in curved ducts and comparison with experimental data
- Computational aerodynamic simulations of a 1215 ft/sec tip speed transonic fan system model for acoustic methods assessment and development
- 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 investigation of tangential slot blowing on a generic chined forebody
- Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
- Computations of axisymmetric flows in hypersonic shock tubes
- Computer code for predicting coolant flow and heat transfer in turbomachinery
- Computer codes for the evaluation of thermodynamic properties, transport properties, and equilibrium constants of an 11-species air model
- Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed
- Conjugate heat transfer analyses on the manifold for ramjet fuel injectors
- Contraction design for small low-speed wind tunnels
- Convective heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis icing research tunnel
- Correlation of puma airloads : evaluation of CFD prediction methods
- Current Lewis turbomachinery research : building on our legacy of excellence
- Current Lewis turbomachinery research : building on our legacy of excellence
- Data Parallel Line Relaxation (DPLR) code user manual : Acadia version 4.01.1
- Demonstration of separation delay with glow-discharge plasma actuators
- Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel
- Design and analysis tool for external-compression supersonic inlets
- Design and calibration of the mixing layer and wind tunnel
- Deterministic stress modeling of hot gas segregation in a turbine
- Development of an actuator for flow control utilizing detonation
- Development of detonation modeling capabilities for rocket test facilities : hydrogen-oxygen-nitrogen mixtures
- Development of tripropellant CFD design code : contract no.--NAS8-40583 : final report
- Discrete-vortex model for the symmetric-vortex flow on cones
- Dynamic flow management problems in air transportation
- Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach
- Effect of delta tabs on free jets from complex nozzles
- Effect of delta tabs on free jets from complex nozzles
- Effect of sweep on cavity flow fields at subsonic and transonic speeds
- Effects of convection during the photodeposition of polydiacetylene thin films
- Effects of gravity on cocurrent two-phase gas-liquid flows through packed columns
- Effects of gravity on cocurrent two-phase gas-liquid flows through packed columns
- Effects of inlet flow conditions on crossflow jet mixing
- Effects of inlet flow conditions on crossflow jet mixing
- Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows : progress report for the period ended December 31, 1989
- Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance
- Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825
- Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79
- Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
- Electron-beam diagnostic methods for hypersonic flow diagnostics : final NASA report grant no. 2-718
- Endwall heat transfer measurements in a transonic turbine cascade
- Endwall heat transfer measurements in a transonic turbine cascade
- Endwall heat transfer measurements in a transonic turbine cascade
- Energy efficient engine : high pressure turbine component test performance report
- 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 line integral convolution with flow feature detection : NAS technical report NAS-96-007
- Equilibrium radiative heating tables for aerobraking in the Martian atmosphere
- Equilibrium radiative heating tables for earth entry
- Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight
- Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight
- Evaluation of non-intrusive flow measurement techniques for a re-entry flight experiment
- Evaluation of turbulence models for unsteady flows of an oscillating airfoil
- Evolution toward a decentralized air traffic flow management system : final report
- Evolutionary concepts for decentralized air traffic flow management
- Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes
- Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft
- Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly
- 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 crater growth dynamics : semiannual report
- Experimental investigation of hexcomb-pattern roughness effects on transition onset and turbulent heating augmentation at Mach 6
- Experimental investigation of the flow field in a transonic, axial flow compressor, with respect to the development of blockage and loss
- Experimental study of saddle point of attachment in laminar juncture flow
- Experimental visualization of flows in packed beds of spheres
- Experimental visualization of flows in packed beds of spheres
- Exploring a method for improving turbulent separated-flow predictions with [k-omega] models
- Extension of a streamwise upwind algorithm to a moving grid system
- Extension of a three-dimensional viscous wing flow analysis
- Final report on investigation of transonic flow over segmented slotted wind tunnel wall with mass transfer
- Final report, entitled, Data reduction and analysis of Pioneer Venus Orbital Ion Mass Spectrometer : NASA grant NAG 2-566, covering the period October 1998 - March 1996
- Final report, entitled, Data reduction and analysis of Pioneer Venus Orbital Ion Mass Spectrometer : NASA grant NAG 2-566, covering the period October 1998 - March 1996
- Final technical report for Euler/Navier-Stokes solvers applied to ducted fan configurations : NASA grant number NAG3-1230 : grant duration, December 20, 1990 to December 20, 1996
- Flight test results from the rake airflow gage experiment on the F-15B airplane
- Flow distribution around the SSME main injector assembly using porosity formulation
- Flow duct data for validation of acoustic liner codes for impedance education
- Flow field around a hovering rotor
- Flow field characterization of an angled supersonic jet near a bluff body
- Flow fields of low pressure vent exhausts
- Flow in rotating serpentine coolant passages with skewed trip strips : under contract NAS3-27378
- Flow quality studies of the NASA Glenn Research Center Icing Research Tunnel circuit (1995 tests
- Flow quality studies of the NASA Glenn Research Center Icing Research Tunnel circuit (1995 tests)
- Flow simulation in secondary flow passages of a rocket engine turbopump : draft paper for 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 13-15, 1998, Cleveland, Ohio
- Flow through very porous screens
- Flow-field surveys for rectangular nozzles
- Flowfield computation of entry vehicles
- Flowfield-dependent mixed explicit-implicit (FDMEI) algorithm for computational fluid dynamics : final report ...
- Flows in pinned arrays simulating brush seals
- Flows in pinned arrays simulating brush seals
- Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines
- Further developments of the fringe-imaging skin friction technique
- Global flowfield about the V-22 tiltrotor aircraft : final report of NASA cooperative agreement NCC2-747
- Growth characteristics downstream of a shallow bump : computation and experiment
- Harmonic balance computations of fan aeroelastic stability
- Heat entrapment effects within liquid acquisition devices
- Heat entrapment effects within liquid acquisition devices
- High pressure turbine test hardware detailed design report
- High resolution Euler solvers based on the space-time conservation element and solution element method
- High speed turboprop aeroacoustic study (counterrotation), Volume 1, Model development
- High-altitude plume computer code development : final report
- Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnel
- Hybrid propulsion for launch vehicle boosters : a program status update
- Hypersonic boundary-layer transition for X-33 phase II vehicle
- Hypervelocity atmospheric flight : real gas flow fields
- ICEG2D (v2.0 : an integrated software package for automated prediction of flow fields for single-element airfoils with ice accretion
- Ice particle transport analysis with phase change for the E3 turbofan engine using LEWICE3D version 3.2
- Identification and characterization of key human performance issues and research in the Next Generation Air Transportation System (NextGen)
- Implementation of an associative flow rule including hydrostatic stress effects into the high strain rate deformation analysis of polymer matrix composites
- Improving jet reactor configuration for production of carbon nanotubes
- Influence of two-phase thermocapillary flow on cryogenic liquid retention in microscopic pores
- Injector mixing efficiency experiments : final report : contract number NAS8-38609 D.O. 159
- Inlet flow control and prediction technologies for embedded propulsion systems : summary report for fiscal year 2009
- Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems : final report, Task 1, Ducted propfan analysis
- Investigation of mixing a supersonic stream with the flow downstream of a wedge : NCC2-5190 final report
- Jet noise physics and modeling using first-principles simulations
- Jet noise reduction potential from emerging variable cycle technologies
- Jet vortex generators for turbulent flow separation control
- Key topics for high-lift research : a joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996
- LAURA users manual, 5.3-48528
- 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
- Lateral jet injection into typical combustor flowfields
- Local and global bifurcations of flow fields during physical vapor transport : application to a microgravity experiment
- Local and global bifurcations of flow fields during physical vapor transport : application to a microgravity experiment
- Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds
- Low speed calibration of the NASA Lewis Research Center 8- by 6-foot supersonic wind tunnel (1995 test) : under contract NAS3-27186
- Mach 10 experimental database of a three-dimensional scramjet inlet flow field
- Mach 5 inlet CFD and experimental results
- Mach 6 flow field surveys beneath the forebody of an airbreathing missile
- Magnetohydrodynamic and gasdynamic theories for planetary bow waves
- Measured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet
- Measurements and simulations of surface dielectric barrier discharges used as plasma actuators, final report
- Measurements of a single lateral jet injected into swirling crossflow
- Measurements of a turbulent horseshoe vortex formed around a cylinder
- Measurements of heat transfer, flow, and pressures in a simulated turbine blade internal cooling passage
- Measurements of turbulent flow field in separate flow nozzles with enhanced mixing devices, test report
- Micro-ramp flow control for oblique shock interactions : comparisons of computational and experimental data
- Navier-Stokes calculations for a highly-twisted rotor near stall
- Near-wall modelling of compressible turbulent flows : a semi-annual progress report
- Nonequilibrium radiation and chemistry models for aerocapture vehicle flowfields : semiannual progress report, February 1991 - June 1991
- Nonequilibrium radiation and chemistry models for aerocapture vehicle flowfields : semiannual progress report, January 1990--June 1990
- Nonlinear dynamics of a diffusing interface
- Numerical analysis of base flowfield for a four-engine clustered nozzle configuration
- Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers
- Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers
- 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 investigation of hot gas ingestion by STOVL aircraft : prepared under grant NAG3-1026
- 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 fluctuations leading to noise in a flap-edge flowfield
- Numerical simulation of particle-wave interaction in boundary layers : final report for NAG-1-798
- Numerical solution of three-dimensional unsteady transonic flow over wings including viscid/viscous interactions
- Numerical solutions of atmospheric flow over semielliptical simulated hills
- Numerical solutions of the complete Navier-Stokes equations : final report : NASA grant NAG-1-244
- Numerical study of steady and unsteady canard-wing-body aerodynamics
- On approximate factorization schemes for solving the full potential equation
- On approximate factorization schemes for solving the full potential equation
- On computations of the integrated space shuttle flowfield using overset grids : final report
- On hammershock propagation in a supersonic flow field
- On multiple-layered vortices
- On the coupling of CDISC design method with FPX rotor code
- On the receptivity and non-parallel stability of traveling disturbances in rotating disk flow
- Optical and probe determination of soot concentrations in a model gas turbine combustor
- Optimum shape of a blunt forebody in hypersonic flow
- PIV and rotational raman-based temperature measurements for CFD validation of a perforated plate cooling flow : part 1
- Parallel ALLSPD-3D : speeding up combustor analysis via parallel processing
- Parallelizing Navier-Stokes computations on a variety of architectural platforms
- 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 improvement through indexing of turbine airfoils, Part 2, Numerical simulation
- Performance tests for the NASA Ames Research Center 20 cm x 40 cm oscillating flow wind tunnel : progress report
- Phase averaged measurements of the coherent structure of a Mach number 0.6 jet
- Physical vapor transport of mercurous chloride under a nonlinear thermal profile
- Physics based model for cryogenic chilldown and loading, Part IV, Code structure
- Plume dispersion of the exhaust from a cryogenic wind tunnel
- Predicting modes of the unsteady vorticity field near the trailing edge of a blade
- Pressure probe designs for dynamic pressure measurements in a supersonic flow field
- Pressure-distribution measurements on a transonic low-aspect ratio wing
- Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane
- RNS applications for interacting sub- and supersonic flows : final report, NASA grant no. NAG1-1553, 11/19/93-5/18/97
- RSRM 10% Scale Model drilled hole plate tests : final report, contract NAS8-40347
- Radiation from advanced solid rocket motor plumes
- Real gas effects on the performance of hydrocarbon-fueled pulse detonation engines
- Real-gas flow properties for NASA Langley Research Center Aerothermodynamic Facilities Complex wind tunnels : under grants NAG1-1663 and NAGW-1331
- Refraction of sound emitted near solid boundaries from a sheared jet
- Response of high subsonic jet to nonaxisymmetric disturbances
- Results of the AFRSI rewaterproofing systems screening test in the NASA/AMES Research Center (ARC) 2x2-foot transonic wind tunnel (OS-310
- Review of blunt body wake flows at hypersonic low density conditions
- Review of blunt body wake flows at hypersonic low density conditions
- Rocket-based combined cycle engine technology development : inlet CFD validation and application
- SSME LOX post flow analysis/fluid structure interaction : final report
- SSME LOX post flow analysis/fluid structure interaction : final report, Volume 1, Flow analysis
- Self-recirculating casing treatment concept for enhanced compressor performance
- Semi-annual status report on NASA grant NAG 1-1087 : "identification of aerodynamic models for maneuvering aircraft"
- Semianalytic modeling of aerodynamic shapes
- Semidiscrete Galerkin modelling of compressible viscous flow past a circular cone at incidence
- Shear layer excitation, experiment versus theory
- 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 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
- Solutions to three-dimensional thin-layer Navier-Stokes equations in rotating coordinates for flow through turbomachinery
- Some aspects of essentially nonoscillatory (ENO) formulations for the Euler equations
- Stability of a non-orthagonal stagnation flow to three dimensional disturbances
- Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct
- Structure of a swirl-stabilized combusting spray
- Study of CFD methods applied to rapidly deforming boundaries
- Study of the integration of wind tunnel and computational methods for aerodynamic configurations
- Study of the unsteady flow features on a stalled wing
- Subsonic aerodynamic assessment of vortex flow management devices on a high-speed civil transport configuration
- Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
- Summary of in-flight flow visualization obtained from the NASA high alpha research vehicle
- Summary of pressure gain combustion research at NASA
- Supersonic retropropulsion test 1853 in NASA LaRC Unitary Plan Wind Tunnel test section 2
- Surface tension driven convection experiment (STDCE)
- Survey of turbulence models for the computation of turbulent jet flow and noise
- System identification and POD method applied to unsteady aerodynamics
- TAS- a transonic aircraft/store flow field prediction code
- The F/A-18 high-angle-of-attack ground-to-flight correlation : lessons learned
- The F/A-18 high-angle-of-attack ground-to-flight correlation, lessons learned
- The determination of the large-scale circulation of the Pacific Ocean from satellite altimetry using model Green's functions
- The effect of incoming boundary layer characteristics on the performance of a distributed propulsion system
- The effect of vortex generators on a jet in a cross-flow
- The effect of wake passing on turbine blade film cooling
- The effect of wake passing on turbine blade film cooling
- The effects of forcing on a single stream shear layer and its parent boundary layer
- The physics of turbulence in the boundary layer : final report ... NASA grant NAG-1-1610
- The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios
- Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels
- Three-dimensional Euler time accurate simulations of fan rotor-stator interactions
- Three-dimensional flow field measurements in a transonic turbine
- Three-dimensional flow field measurements in a transonic turbine cascade
- Thrust measurement of Dielectric Barrier Discharge (DBD) plasma actuators : new anti-thrust hypothesis, frequency sweeps methodology, humidity and enclosure effects
- Towards a comprehensive computational simulation system for turbomachinery
- Transition and turbulence modeling for blunt-body wake flows : abstract of paper proposed for the 32nd AIAA Thermophysics Conference, June 23-25, 1997, Atlanta, Georgia
- Transition mixing study final report
- Turbulence modeling validation, testing, and development
- Turbulence modeling validation, testing, and development
- Turbulent chemical interaction models in NCC : comparison
- Turbulent inflow measurements : final report, grant number L-1625, period covered: 5 July 1995 to 31 December 1996
- Two phase flow modeling : summary of flow regimes and pressure drop correlations in reduced and partial gravity
- Understanding and mitigating tip leakage and endwall losses in high pressure ratio cores
- Understanding the flow physics of shock boundary-layer interactions using CFD and numerical analyses
- Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise
- Unsteady flow field in a multistage axial flow compressor
- Unsteady potential flow past a propeller blade section
- Unsteady, transonic flow around delta wings undergoing coupled and natural modes response : a multidisciplinary problem
- Use of a scale model in the design of modifications to the NASA Glenn Icing Research Tunnel
- V/STOL wind-tunnel testing
- Visualization of flows in packed beds of twisted tapes
- Visualization of flows in packed beds of twisted tapes
- Visualizing time-varying phenomena in numerical simulations of unsteady flows
- Visualizing vector fields using line integral convolution and dye advection
- Wake flow about the Mars Pathfinder entry vehicle
- Water flow measurements in a 180 degree turn-around duct
- Water tunnel flow visualization study through poststall of 12 novel planform shapes
- Water tunnel flow visualization study through poststall of 12 novel planform shapes
- Water-tunnel study results of a TF/A-18 and F/A-18 canopy flow visualization
- Wind code application to external forebody flowfields with comparisons to experimental results
- Wind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena

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