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

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

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- 20th International Congress on Instrumentation in Aerospace Simulation Facilities
- 3-D LDV measurements on a 30-degree swept wing with a simulated ice accretion
- A critical assessment of UH-60 main rotor blade airfoil data
- A determination of the external forces required to move the benchmark active controls testing model in pure plunge and pure pitch
- A direct-fire trajectory model for supersonic, transonic, and subsonic projectile flight
- A general multiblock Euler code for propulsion integration, Volume I, Theory document
- A general multiblock Euler code for propulsion integration, Volume II, User guide for BCON, pre-processor for grid generation and GMBE
- A general multiblock Euler code for propulsion integration, Volume III, User guide for the Euler code
- A hybrid numerical technique for predicting the aerodynamic and acoustic fields of advanced turboprops : final report
- A low speed wind tunnel study of vortex interaction control techniques on a chine-forebody/delta-wing configuration
- A mathematical formulation of the SCOLE control problem, Part II, Optimal compensator design
- A new flux splitting scheme
- A nozzle internal performance prediction method
- A numerical simulation of the NFAC (National Full-Scale Aerodynamics Complex) open-return wind tunnel inlet flow
- A study of high speed flows in an aircraft transition duct
- A study on vortex flow control on inlet distortion in the re-engined 727-100 center inlet duct using computational fluid dynamics
- A user guide for the EMTAC-MZ CFD code
- A water tunnel flow visualization study of the vortex flow structures on the F/A-18 aircraft
- Accurate multigrid solution of the Euler equations on unstructured and adaptive meshes
- Adjoint methods for aerodynamic wing design : semi-annual progress report
- Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests)
- Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds
- Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds
- Aerodynamic characteristics and pressure distributions for an executive-jet baseline airfoil section
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept 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 a propeller-powered high-lift semispanwing
- Aerodynamic characteristics of the National Launch System (NLS) 1 1/2 stage launch vehicle
- Aerodynamic design of transport aircraft
- Aerodynamic design of transport aircraft
- Aerodynamic design trends for commercial aircraft
- Aerodynamic generation of sound
- Aerodynamic parameter studies and sensitivity analysis for rotor blades in axial flight
- Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory
- Aerodynamics for engineering students
- Aerodynamics of a sphere and an oblate spheroid for Mach numbers from 0.6 to 10.5 including some effects of test conditions
- Aeroelastic analysis of aircraft : wing and wing/fuselage configurations
- American streamlined design : the world of tomorrow
- An aerodynamic model for one and two degree of freedom wing rock of slender delta wings
- An analysis for high Reynolds number inviscid/viscid interactions in cascades
- An analytical approach to grid sensitivity analysis for NACA four-digit wing sections
- An evaluation in a modern wind tunnel of the transonic adaptive wall adjustment developed by NPL in the 1940's
- An experimental analysis of critical factors involved in the breakdown process of leading edge vortex flows
- An experimental and theoretical study of the aerodynamic characteristics of some generic missles concepts at Mach numbers from 2 to 6.8
- An experimental investigation of S-duct flow control using arrays of low profile vortex generators
- An experimental investigation of a supersonic vortical flow
- An experimental investigation of the aerodynamic characteristics of slanted base ogive cylinders using magnetic suspension technology
- An experimental investigation of the flow in a diffusing S-duct
- An experimental study of airfoil icing characteristics
- An experimental study of natural and forced modes in an axisymmetric jet
- An experimental study of the aerodynamics of a swept and unswept semispan wing with a simulated glaze ice accretion
- An experimental study of the effect of pitch rate on delta wing aerodynamics and stability : for the period April 1, 1986 - June 30, 1988
- An experimental trace gas investigation of fluid transport and mixing in a circular-to-rectangular transition duct
- An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients : semiannual progress report, July 1991- December 1991
- An investigation of the effects of AFT blowing on a 3.0 caliber tangent Ogive body at high angles of attack
- An overview of three approaches to multidisciplinary aeropropulsion simulations
- Analyses and assessments of span wise gust gradient data from NASA B-57B aircraft
- Analysis of a high speed civil transport configuration at subsonic flow conditions using a Navier-Stokes solver
- Applied aerodynamics : challenges and expectations
- Applied hydro- and aeromechanics ; : based on lectures of L. Prandtl
- Applied hydrodynamics
- Atmospheric turbulence, meteorological modeling and aerodynamics
- Atmospheric turbulence, meteorological modeling and aerodynamics
- Automatic computation of Euler-marching and subsonic grids forwing-fuselage configurations
- BANDSLIP advancements
- Bifurcation theory applied to aircraft motions
- Bifurcation theory applied to aircraft motions
- Boundary layer simulator improvement : final report
- Breaking down the delta wing vortex : the role of vorticity in the breakdown
- CFD prediction of Magnus effect in subsonic to supersonic flight
- Calculation of compressible flow about three-dimensional inlets with auxiliary inlets, slats, and vanes by means of a panel method
- Calculations of hot gas ingestion for a STOVL aircraft model
- Calibration apparatus for recess mounted pressure transducers
- Challenges in simulation of aerodynamics, hydrodynamics, and mooring-line dynamics of floating offshore wind turbines
- Comments regarding two upwind methods for solving two-dimensional external flows using unstructured grids
- Comparison of all-electric secondary power systems for civil subsonic transports
- Comparison of numerical flow field predictions for army airdrop systems
- Comparison of theoretical and flight-measured local flow aerodynamics for a low-aspect-ratio fin
- Comparisons of elastic and rigid blade-element rotor models using parallel processing technology for piloted simulations
- Compressibility effects on dynamic stall of airfoils undergoing rapid transient pitching motion
- Computation of three-dimensional effects on two dimensional wings
- Computational design of low aspect ratio wing-winglet configurations for transonic wind-tunnel tests
- Computational results for flows over 2-D ramp and 3-D obstacle with an upwind Navier-Stokes solver
- Conceptual design approach for small-caliber aeroballistics with application to 5.56-mm ammunition
- Confined turbulent swirling recirculating flow predictions
- Control of an axisymmetric turbulent jet by multi-modal excitation
- Control of submersible vortex flows
- Controlling forebody asymmetries in flight : experience with boundary layer transition strips
- Coordinates for a high performance 4:1 pressure ratio centrifugal compressor
- Coupled CFD/GN&C modeling for a smart material canard actuator
- Design and flight evaluation of a new force-based angle probe
- Detailed study of oxidation/wear mechanism in lox turbopump bearings
- Determination of aerodynamic sensitivity coefficients for wings in transonic flow : Leland A. Carlson and Hersham M. El-Banna
- Development of a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) system
- Development of a rotor wake/vortex model
- Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis : semiannual progress report, January 1, 1987 - June 30, 1987
- Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis : semiannual progress report, January 1, 1988 - June 30, 1988
- Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis : semiannual progress report, July 1, 1988 - December 31, 1988
- Development of phased twin flip-flop jets
- Development of selected advanced aerodynamics and active control concepts for commercial transport airfcraft
- Development, analysis and testing of the High Speed Research Flexible Semispan Model
- Dual methods and approximation concepts in structural synthesis
- Dynamic ground effect for a cranked arrow wing airplane
- Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor
- Dynamic response of two composite prop-fan models on a nacelle/wing/fuselage half model
- Dynamics of aerospace vehicles : final technical report
- ERB aerodynamics flow physics facilities
- Effect of 'delta tabs' on mixing and axis switching in jets from asymmetric nozzles
- Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
- Effect of wall cooling on the stability of compressible subsonic flows over smooth humps and backward-facing steps
- Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data
- Elementary matrices and some applications to dynamics and differential equations
- Elements of gasdynamics
- Engine Research Building aeropropulsion heat transfer facilities
- Ethylene trace-gas techniques for high-speed flows
- Euler analysis comparison with LDV data for a advanced counter-rotation propfan at cruise
- Evaluation of four advanced nozzle concepts for short takeoff and landing
- Evaluation of turbulence models in the PARC code for transonic diffuser flows
- Experimental investigation of nozzle/plume aerodynamics at hypersonic speeds
- Experimental investigation of the effects of aft blowing with various nozzle exit geometries on a 3.0 caliber tangent Ogive at high angles of attack : forebody pressure distributions
- Experimental study of a vortex subjected to imposed strain : final report, NASA grant NAG 2-389
- Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
- Experimental verification of a new laminar airfoil : a project for the graduate program in aeronautics : final report
- Exploratory wind-tunnel investigation of a wingtip-mounted vortex turbine for vortex energy recovery
- Figures of merit : remembrances of those who built an Army-NASA collaboration and a new age of rotary-wing technology, 1965-1985
- Figures of merit : remembrances of those who built an Army-NASA collaboration and a new age of rotary-wing technology, 1965-1985
- Final report on an integrated aerodynamic/propulsion study for generic aero-space planes based on waverider concepts
- Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements
- Flight Mechanics/Estimation Theory Symposium, 1990 : proceedings of a symposium sponsored by NASA Goddard Space Flight Center and held at Goddard Space Flight Center, Greenbelt, Maryland, May 22-24, 1990
- Flight dynamics principles
- Flight dynamics principles : [a linear systems approach to aircraft stability and control]
- Flight vehicle aerodynamics
- Flight without formulae ; : simple discussions on the mechanics of the aeroplane
- Flow analysis for the nacelle of an advanced ducted propeller at high angle-of-attack and at cruise with boundary layer control
- Flow through very porous screens
- Fluid dynamics for the study of transonic flow
- Fluid physics
- Forces and pressures induced on circular plates by a single lifting jet in ground effect
- Forebody tangential blowing for control at high angles of attack : feasibility study final report
- Fourth-order 2N Runge-Kutta schemes
- Free-molecule-flow force and moment coefficients of the Aeroassist Flight Experiment vehicle
- Fundamentals of hydro- and aeromechanics : based on lectures of L. Prandtl
- Further development and flight test of an autonomous precision landing system using a parafoil
- Grid generation about complex three-dimensional aircraft configurations : final report
- Grid generation and flow solution method for Euler equations on unstructured grids
- Grid sensitivity for aerodynamic optimization and flow analysis
- HSCT mission analysis of waverider designs : final report, (May 15, 1991 - May 14, 1993)
- HSCT mission analysis of waverider designs : summary of 2nd quarter contract work, (August 15, 1991 - November 15, 1992)
- Hi-alpha forebody design, Part I, Methodology base and initial parametries
- High Reynolds number hybrid laminar flow control (HLFC) flight experiment, II, Aerodynamic design
- High angle-of-attack aerodynamic characteristics of crescent and elliptic wings
- High lift aerodynamics
- High-alpha vortex decoupling investigations on a chine forebody/delta wing configuration at transonic mach numbers
- High-order "cyclo-difference" techniques : an alternative to finite differences
- Hypersonic code efficiency and validation studies
- Hypersonic lateral and directional stability characteristics of aeroassist flight experiment configuration in air and CF4
- Icing characteristics of a natural-laminar-flow, a medium-speed, and a swept,medium-speed airfoil
- Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
- Implicit solvers for unstructured meshes
- Improving diffusing S-duct performance by secondary flow control
- Incompressible viscous flow simulations of the NFAC wind tunnel
- Induced drag ideal efficiency factor of arbitrary lateral-vertical wing forms
- Initial piloted simulation evaluation of the Reference-H High-Speed Civil Transport design during takeoff and recovery from limit flight conditions
- Initial turbulence effect on jet evolution with and without tonal excitation
- Integration of dynamic, aerodynamic, and structural optimization of helicopter rotor blades : final report, NASA research grant no. NAG 1-1710 for period covering 15 October 1986 to 30 November 1991
- Introduction to the aerodynamics of flight
- Inverse boundary-layer theory and comparison with experiment
- Investigation of a FAST-OrcaFlex coupling module for integrating turbine and mooring dynamics of offshore floating wind turbines : preprint
- Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems : task II : unsteady ducted propfan analysis : final report
- Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems : task II, unsteady ducted propfan analysis
- Investigation of advancing front method for generating unstructured grid : progress report for the period ended May 31, 1991
- Investigation of radiative interactions in supersonic internal flows : progress report for the period ended May 31, 1991
- Inviscid instability of streamwise corner flow
- Jet-induced ground effects on a parametric flat-plate model in hover
- LEWICE/E : an Euler based ice accretion code
- Laminar flow control leading edge glove flight test article development
- Langley 14- by 22-foot subsonic tunnel test engineer's data acquisition and reduction manual
- Large amplitude acoustic excitation of swirling turbulent jets
- LinAir:a multi-element discrete vortex Weissinger aerodynamic prediction method
- Linear theory of a dual-spin projectile in atmospheric flight
- Low-speed longitudinal aerodynamic characteristics of a flat-plate planform model of an advanced fighter configuration
- Low-speed longitudinal and lateral-directional aerodynamic characteristics of the X-31 configuration
- Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
- Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels
- Ludwig Prandtl collected treatises on applied mechanics, hydro- and aerodynamics, Part 1
- Ludwig Prandtl collected treatises on applied mechanics, hydro- and aerodynamics, Part 2, IV, Interfaces and resistance
- Methods of applied dynamics
- Micro-optical distributed sensors for aero propulsion applications
- Micro-optical distributed sensors for aero propulsion applications
- Mixing noise reduction for rectangular supersonic jets by nozzle shaping and induced screech mixing
- Modeling and simulation of a differential roll projectile
- Multiaxis thrust vectoring using axisymmetric nozzles and postexit vanes on an F/A-18 configuration vehicle
- Multidisciplinary design optimization using multiobjective formulation techniques : final report on NASA Ames grant no. NCA2-778
- NASA low-speed centrifugal compressor for 3-D viscous code assessment and fundamental flow physics research
- Navier-Stokes calculations of scramjet-nozzle-afterbody flowfields
- Nonlinear aerodynamics and the design of wing tips
- Nonlinear aerodynamics and the design of wing tips : final report, year 1 ... covering the period April 1, 1990 to March 31, 1991
- Nonlinear interaction of near-planar TS waves and longitudinal vortices in boundary-layer transition
- Numerical computation of complex multi-body compressible Navier-Stokes flows with applications for the integrated space shuttle vehicle
- Numerical investigation of plasma actuator configurations for flow separation control at multiple angles of attack
- Numerical methods for the simulation of complex multi-body flows with applications for the Integrated Space Shuttle Vehicle
- Numerical study of boundary-layer control in aerodynamics : final technical report for grant NCC 2-845, NASA-Ames Research Center; grant period: 1 January 1994 to 31 December 1995, no-cost extension to 31 December 1996
- On simple aerodynamic sensitivity derivatives for use in interdisciplinary optimization
- On the estimation algorithm used in adaptive performance optimization of turbofan engines
- On the nonlinear stability of a high-speed, axisymmetric boundary layer
- On the nonlinear three-dimensional instability of Stokes layers and other shear layers to pairs of oblique waves
- Operational aerodynamic data book
- PAN AIR, a computer program for predicting subsonic or supersonic linear potential flows about arbitrary configurations using a higher order panel method
- PROFILE : airfoil geometry manipulation and display : user's guide
- Parallel visualization of large-scale aerodynamics calculations : a case study on the Cray T3E
- Parallelization of a parabolized Navier-Stokes solver with a design optimizer : 34th AIAA Aerospace Sciences Meeting and Exhibit
- Parameter identification for nonlinear aerodynamic systems
- Parameter identification for nonlinear aerodynamic systems : final technical report to the Aircraft Guidance and Controls Branch/489, Guidance and Control Division, National Aeronautics and Space Administration, Langley Research Center ... period covered, October 23, 1989 to February 28, 1993
- Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20
- Parametric study of a canard-configured trasport using conceptual design optimization
- Particle kinetic simulation of high altitude hypervelocity flight
- Particle kinetic simulation of high altitude hypervelocity flight : periodic research report for the period February 1, 1992 - December 31, 1992
- Particle trajectory computer program for icing analysis of axisymmetric bodies : final report
- Physical sciences informatics system
- Piloted simulation study of an ILS approach of a twin-pusher business/commuter turboprop aircraft configuration
- Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap
- Prediction of vortex shedding from circular and noncircular bodies in subsonic flow
- Predictive wall adjustment strategy for two-dimensional flexible walled adaptive wind tunnel : a detailed description of the first one-step method
- Pressure distribution for the wing of the YAV-8B airplane ; with and without pylons
- Pressure-sensing performance of upright cylinders in a Mach-10 boundary layer
- Principles of ideal-fluid aerodynamics
- Program of research in flight dynamics in the JIAFS at NASA-Langley Research Center : NASA cooperative agreement, NCC2-29, annual status report, December 1, 1991 - November 30, 1992
- Radiative energy transfer in molecular gases
- Radiative interactions in chemically reacting supersonic internal flows
- Rarefied-flow aerodynamics : final summary report, NASA research grant NAG-1-921, 1 January 1989 to 31 May, 1992
- Rectangular subsonic jet flow field measurements
- Reduction of structural loads using the maneuver load control on the advanced fighter technology integration (AFTI)/F-111 mission adaptive wing
- Results of the 1987 NASA/JPL balloon flight solar cell calibration program
- Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90°
- STARS, an integrated, multidisciplinary, finite-element, structural, fluids, aeroelastic, and aeroservoelastic analysis computer program
- Sailing aerodynamics
- Semi-span model testing in the National Transonic Facility : annual status report, October 1993, cooperative agreement no. NCC1, 169
- Semiannual progress report no. 4 to Aircraft Guidance and Controls Branch/489 Guidance and Control Division, National Aeronautics and Space Administration, Langley Research Center ... for the grant parameter identification for nonlinear aerodynamic systems... : period covered, April 24, 1991 to October 22, 1991
- Sensitivity analysis of dynamic aeroelastic responses in transonic flow
- Simple aerodynamics and the airplane
- Simplified, inverse, ejector design tool
- Simulation of unsteady rotational flow over propfan configuration
- Small-scale experiments in STOVL ground effects
- Some VTOL head-up display drive-law problems and solutions
- Sound propagation studies for a large horizontal axis wind turbine
- Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities
- Steady pressure measurements on an aeroelastic research wing (ARW-2)
- Structural shape optimization in multidisciplinary system synthesis
- Subsonic aerodynamic characteristics of semispan commercial transport model with wing-mounted advanced ducted propeller operating in reverse thrust
- Subsonic aerodynamic characteristics of the HL-20 lifting-body configuration
- Subsonic flight test evaluation of a propulsion system parameter estimation process for the F-100 engine
- Subsonic investigations of vortex interaction control for enhanced high-alpha aerodynamics of a chine forebody/delta wing configuration
- Suckdown, fountain lift, and pressures induced on several tandem jet V/STOL configurations
- Supersonic flow with feeding of energy
- Techniques for estimating space station aerodynamic characteristics, July 1, 1989 - August 31, 1992
- The Aero-Acoustic Propulsion Laboratory
- The Encyclopedia of Aerodynamics
- The dynamics and control of fluctuating pressure loads in the reatachment region of a supersonic free shear layer
- The illustrated guide to aerodynamics
- The measurement of disturbance levels in the Langley Research Center 20-inch Mach 6 tunnel
- The mechanics of the aeroplane : a study of the principles of flight
- The regional nature of aerodynamic jump
- The resistance of the air and aviation ; : experiments conducted at the Champs-de-mars laboratory
- The streamline era
- The theory of thin wings in subsonic flow
- Theoretical investigation of non-equilibrium chemistry and optical radiation in hypersonic flow fields
- Third-order 2N Runge-Kutta schemes with error control
- Three-dimensional singular points in aerodynamics
- Time-accurate numerical prediction of free flight aerodynamics of a finned projectile
- Topics in advanced model rocketry
- Trajectory optimization and guidance law development for national aerospace plane applications : final report, July 1, 1987 to November 30, 1988
- Transient Ejector Analysis (TEA) code user's guide
- Transition aerodynamics for 20-percent-scale VTOL unmanned aerial vehicle
- Transonic dynamics tunnel force and pressure data acquired on the HSR rigid semispan model
- Turbulence characteristics of swirling flowfields
- Turbulent swirling jets with exitation
- Ultra high bypass nacelle aerodynamics : inlet flow-through high angle of attack distortion test
- Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise
- Unstructured and adaptive mesh algorithms for aerodynamic calculations
- Unstructured-grid methods development, lessons learned
- User's guide for a "flat wake" rotor inflow/wake velocity prediction code, "down"
- User's manual for AeroFcn : a FORTRAN program to compute aerodynamic parameters
- Verification of performance results for a low-speed 15% eliptical circulation control airfoil
- Vortex breakdown and control experiments in the Ames-Dryden water tunnel
- Wind tunnel aerodynamic characteristics of a transport-type airfoil in a simulated heavy rain environment
- Wind tunnel investigations of forebody strakes for yaw control on F/A-18 model at subsonic and transonic speeds
- Wing theory
- Wing theory
- X-29 flight control system : lessons learned
- X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results

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