#
Aerodynamics
Resource Information
The concept ** Aerodynamics** represents the subject, aboutness, idea or notion of resources found in **Houston Public Library**.

The Resource
Aerodynamics
Resource Information

The concept

**Aerodynamics**represents the subject, aboutness, idea or notion of resources found in**Houston Public Library**.- Label
- Aerodynamics

## Context

Context of Aerodynamics#### Subject of

- 3-D LDV measurements on a 30-degree swept wing with a simulated ice accretion
- A Collection of flow visualization techniques used in the aerodynamic research branch
- A Numerical simulation of three-dimensional flow in an adaptive wall wind tunnel
- A Perspective of computational fluid dynamics
- A comparison of the pitching and plunging response of an oscillating airfoil
- A comparison of the results of dynamic wind-tunnel test with theoretical predictions for an aeromechanical gust-alleviation system for light airplanes
- A computer program to generate equations of motion matrices, L217 (EOM)
- A consistent spatial differencing scheme for the transonic full-potential equation in three dimensions
- A critical assessment of UH-60 main rotor blade airfoil data
- A critical assessment of wind tunnel results for the NACA 0012 airfoil
- A determination of the external forces required to move the benchmark active controls testing model in pure plunge and pure pitch
- 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 geometry package for generation of imput data for a three-dimensional potenial-flow program
- 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 natural low frequency oscillation in the wake of an airfoil near stalling conditions
- 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 program to compute three-dimensional subsonic unsteady aerodynamic characteristics using the doublet lattice method, L216 (DUBFLX)
- A review of some Reynolds number effects related to bodies at high angles of attack
- A spatial model of wind shear and turbulence for flight simulation
- A study of flow past an airfoil with a jet issuing from its lower surface
- A study of high speed flows in an aircraft transition duct
- A study of panel loads and centers of pressure of three different cruciform aft-tail control surfaces of a wingless missile from March 1.60 to 3.70
- A study on vortex flow control on inlet distortion in the re-engined 727-100 center inlet duct using computational fluid dynamics
- A three dimensional vortex wake model for missiles at high angles of attack
- A throat-bypass stability-bleed system using relief valves to increase the transient stability of a mixed-compression inlet
- A user guide for the EMTAC-MZ CFD code
- A viscous flow analysis for the tip vortex generation process
- 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
- Acquisition and utilization of wind tunnels by the National Aeronautics and Space Administration : report to the Committee on Science and Technology, House of Representatives
- Adjoint methods for aerodynamic wing design : semi-annual progress report
- Advanced missile technology : a review of technology improvement areas for cruise missiles
- 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 characteristcs of a propeller-powered high-lift semispanwing
- Aerodynamic characteristics and pressure distributions for an executive-jet baseline airfoil section
- Aerodynamic characteristics of a high-wing transport configuration with an over-the-wing Nacelle-pylon arrangement
- Aerodynamic characteristics of a hypersonic cruise aircraft concept with wing-mounted propulsion systems at mach numbers of 2.96, 3.96, and 4.63
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0
- 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 series of twin-inlet air-breathing missile configurations
- Aerodynamic characteristics of an air-exchanger system for the 40-by 80-foot wind tunnel at Ames Research Center
- Aerodynamic characteristics of forebody and nose strakes based on F-16 wind tunnel test experience ; prepared for Langley Research Center under contract NAS1-15006
- Aerodynamic characteristics of sixteen electric, hybrid, and subcompact vehicles : complete data
- Aerodynamic characteristics of the 140A/B space shuttle orbiter at Mach 10.3
- Aerodynamic characteristics of the National Launch System (NLS) 1 1/2 stage launch vehicle
- Aerodynamic characteristics of the standard dynamics model in coning motion at Mach 0.6
- Aerodynamic design trends for commercial aircraft
- Aerodynamic interactions from reaction controls for lateral control of the M2-F2 lifting-body entry configuration at transonic and supersonic mach numbers
- Aerodynamic parameter studies and sensitivity analysis for rotor blades in axial flight
- Aerodynamic performance of 0.4066-scale model of JT8D refan stage
- Aerodynamic performance of flared fan nozzles used as inlets
- Aerodynamic performance of the 17-M-diameter Darrieus wind turbine in the three-bladed configuration : an addendum
- Aerodynamic performance of the 17-metre-diameter Darrieus wind turbine
- Aerodynamic properties of a flat plate with cavity for optical-propagation studies
- Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory
- Aerodynamic theory : a general review of progress
- Aerodynamics of a sphere and an oblate spheroid for Mach numbers from 0.6 to 10.5 including some effects of test conditions
- Aerodynamics of seeing on large transport aircraft : final technical report, 1 December 1985 through 30 November 1986
- Aerodynamics/ACEE
- Aeroelastic addition to NASTRAN
- Aeroelastic addition to NASTRAN
- Aeronautical facilities catalogue
- Air Disasters
- Aircraft control by propeller cyclic blades
- American streamlined design
- An Improved panel method for the solution of three-dimensional leading-edge vortex flows
- 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 analysis of the viscous flow through a compact radial turbine by the average passage approach
- An analytical approach to grid sensitivity analysis for NACA four-digit wing sections
- An entropy correction method for unsteady full potential flows with strong shocks
- 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 investigation of the effect of nonmetric over-the-wing nacelles on wing-body aerodynamics
- An experimental and theoretical investigation of thick wings at various sweep angles in and out of ground effect
- 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 free-tip response to a jet
- An experimental investigation of multi-element airfoil ice accretion and resulting performance degradation
- An experimental investigation of the aerodynamic characteristics of slanted base ogive cylinders using magnetic suspension technology
- An experimental investigation of the aerodynamics and cooling of a horizontally-opposed air-cooled aircraft engine installation
- An experimental investigation of the aerodynamics of a NACA 64A010 airfoil-flap combination with and without flap oscillations : Part 1, Steady-state characteristics
- An experimental investigation of the flap-lag-torsion aeroelastic stability of a small-scale hingeless helicopter rotor in hover
- An experimental investigation of the flow in a diffusing S-duct
- An experimental investigation of thrust vectoring two-dimensional convergent-divergent nozzles installed in a twin-engine fighter model at high angles of attack
- 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 experimental wind-tunnel investigation of a ram-air-spoiler roll-control device on a forward-control missile at supersonic speeds
- An exploratory investigation of the STOL landing maneuver
- An improved Woodward's panel method for calculating leading-edge and side-edge suction forces at subsonic and supersonic speed
- 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 unsteady helicopter rotor-fuselage interaction analysis
- 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
- Analysis of nonplanar wing-tip-mounted lifting surfaces on low-speed airplanes
- Analytical and experimental study of flow phenomena in noncavitating rocket pump inducers
- Analytical modeling of circuit aerodynamics in the new NASA Lewis Altitude Wind Tunnel
- Analytical modeling of helicopter static and dynamic induced velocity in grasp
- Analytical study of a free-wing/free-trimmer concept
- Applicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edges
- Application of Runge Kutta time marching scheme for the computation of transonic flows in turbomachines
- Application of a lower-upper implicit scheme and an interactive grid generation for turbomachinery flow field simulations
- Application of empirical and linear methods to VSTOL powered-lift aerodynamics
- Application of the Bernoulli enthalpy concept to the study of vortex noise and jet impingement noise
- Applied aerodynamics : challenges and expectations
- Applied aerodynamics,
- Approximation concepts for numerical airfoil optimization
- Automated reduction of data from images and holograms :
- Automatic computation of Euler-marching and subsonic grids forwing-fuselage configurations
- Autonomous momentum management for space station : final report, 15 October 1984
- Bifurcation analysis of aircraft pitching motions near the stability boundary
- 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
- Calculation of aerodynamic characteristics of airplane configurations at high angles of attack
- Calculation of compressible flow about three-dimensional inlets with auxiliary inlets, slats, and vanes by means of a panel method
- Calculation of steady and unsteady airfoil flow fields via the Navier-Stokes equations
- Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects : User's manual
- Calculation of two-dimensional inlet flow fields in a supersonic free stream : program documentation and test cases
- Calculations of hot gas ingestion for a STOVL aircraft model
- Calibration apparatus for recess mounted pressure transducers
- Characteristics of loaded fan rotor blade wakes
- Classical aerodynamic theory
- Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine : II - effect of air ejection on turbine performance
- Combined aerodynamic and structural dynamic problem emulaing routines (CASPER) : theory and implementation
- 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 experimental surface pressure with theoretical predictions on twin two-dimensional convergent-divergent nozzles
- 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
- Computation of three-dimensional nozzle-exhaust flow fields with the GIM code / L. W. Spradley, P. G. Anderson, and M. L. Pearson
- Computational design of low aspect ratio wing-winglet configurations for transonic wind-tunnel tests
- Computational model for vortex generators in subsonic internal flows
- Computational results for flows over 2-D ramp and 3-D obstacle with an upwind Navier-Stokes solver
- Computer program to calculate three-dimensional boundary layer over wings with wall mass transfer
- Confined turbulent swirling recirculating flow predictions
- 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
- Crossflow vorticity sensor : patent application
- Design and analysis of advanced flight planning concepts
- 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 and validation of an advanced low-order panel method
- Development of a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) system
- 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, July 1, 1988 - December 31, 1988
- Development of panel methods for subsonic analysis and design
- Development of phased twin flip-flop jets
- Development of selected advanced aerodynamics and active control concepts for commercial transport airfcraft
- Downwash in the plane of symmetry of an elliptically loaded wing
- Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers
- Dual methods and approximation concepts in structural synthesis
- Dual methods and approximation concepts in structural synthesis
- Dynamic characteristics of a space-station solar wing array
- Dynamic response of some tentative compliant wall structures to convected turbulence fields
- Dynamic response of two composite prop-fan models on a nacelle/wing/fuselage half model
- Dynamics of Atmospheric Flight
- 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 blade planform variation on a small-scale hovering rotor
- Effect of canard vertical location, size, and deflection on canard-wing interference at subsonic speeds
- Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes : I--performance with coolant ejection holes plugged
- Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes : II-performance with coolant flow ejection at temperature ratios up to 2
- Effect of deflected thrust on the longitudinal aerodynamic chartacteristics of a close-coupled wing-canard configuration
- Effect of design changes on aerodynamic and acoustic performance of translating centerbody sonic inlets
- Effect of nose bluntness and afterbody shape on aerodynamic characteristics of a monoplanar missile concept with bodies of circular and elliptical cross sections at a mach number of 2.50
- Effect of pylon wake with and without pylon blowing on propeller thrust
- Effect of wall cooling on the stability of compressible subsonic flows over smooth humps and backward-facing steps
- Effects of body shape on the aerodynamics of a body of revolution at Mach numbers from 1.6 to 4.6
- Effects of conventional and square stores on the longitudinal aerodynamic characteristics of a fighter aircraft model at supersonic speeds
- Effects of nacelle configuration/position on performance of subsonic transport
- Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles
- Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds
- Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane
- Effects of turbulence and delay in activating TIGER II after low altitute release
- Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data
- Efficient real gas Navier-Stokes computations of high speed flows using an LU scheme
- Efficient solutions to the Euler equations for supersonic flow with embedded subsonic regions
- Engine Research Building aeropropulsion heat transfer facilities
- Environmental effects on space shuttle reusable surface insulation coated with reaction cured glass
- 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 aerodynamic characteristics for slender bodies with thin wings and tail at angles of attack from 0 ̊to 58 ̊and Mach from 0.6 to 2.0
- Experimental aerodynamic characteristics of a joined-wing research aircraft configuration
- Experimental determination of flow-interference effects of wing-mounted two-dimensional, full-capture propulsion nacelles in close proximity to a vehicle body at a Mach number of 6
- Experimental evaluation of nacelle-airframe interference forces and pressures at Mach numbers of 0.9 to 1.4
- 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 verification of a new laminar airfoil : a project for the graduate program in aeronautics : final report
- Exploratory studies of the cruise performance of upper surface blown configurations : experimental program : test facilities, model design, instrumentation, and low-speed, high-lift tests
- Exploratory studies of the cruise performance of upper surface blown configurations : summary report
- Exploratory wind-tunnel investigation of a wingtip-mounted vortex turbine for vortex energy recovery
- Final report on an integrated aerodynamic/propulsion study for generic aero-space planes based on waverider concepts
- Finite element analysis of low speed viscous and inviscid aerodynamic flows
- Finite-difference computations of rotor loads
- Fitting aerodynamic forces in the Laplace domain : an application of a nonlinear nongradient technique to multilevel constrained optimization
- 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
- Flow visualization studies of a general research fighter model employing a strake-wing concept at subsonic speeds
- Flutter analysis of highly swept delta wings by conventional methods
- Flutter and forced response of mistuned rotors using standing wave analysis
- 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
- Fuel efficiency through new airframe technology
- 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
- Ground effects on V/STOL and STOL aircraft--a survey
- Gust load estimation using a simplified power spectral technique
- 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)
- Helicopter hub fairing and pylon interference drag
- Hi-alpha forebody design, Part I, Methodology base and initial parametries
- High Reynolds number tests of a Douglas DLBA 032 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- 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
- Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition
- Homing performance comparison of selected airframe configurations using skid-to-turn and bank-to-turn steering policies
- Hot gas ingestion testing of an advanced STOVL concept in the NASA Lewis 9- by 15-foot low speed wind tunnel with flow visualization
- Hub loads analysis of the SA349/2 helicopter
- Hybrid laminar flow control study final technical report : energy efficient transport program
- Hypersonic code efficiency and validation studies
- Hypersonic lateral and directional stability characteristics of aeroassist flight experiment configuration in air and CF6
- Icing characteristics of a natural-laminar-flow, a medium-speed, and a swept,medium-speed airfoil
- Image processing of aerodynamic data
- Implementation of uniform perturbation method for potential flow past axisymmetric and two-dimensional bodies
- Implicit solvers for unstructured meshes
- Improvement of maneuver aerodynamics by spanwise blowing
- Improving diffusing S-duct performance by secondary flow control
- Incompressible lifting-surface aerodynamics for a rotor-stator combination
- Incompressible viscous flow simulations of the NFAC wind tunnel
- Induced drag ideal efficiency factor of arbitrary lateral-vertical wing forms
- Inflow measurement made with a laser velocimeter on a helicopter model in forward flight : Volume V, Tapered planform blades at an advance ratio of 0.23
- Influence of aerodynamic phenomena on pollutant formation in combustion
- Influence of base modifications on in-flight base drag in the presence of jet exhaust for Mach numbers from 0.7 to 1.5
- Influence of surface static-pressure orifices on boundary-layer transition
- Influence of wind shear on the aerodynamic characteristics of airplanes
- Initial turbulence effect on jet evolution with and without tonal excitation
- Integrated application of active controls (IAAC) technology to an advanced subsonic transport project : current and advanced act control system definition study : final report
- Integrated application of active controls (IAAC) technology to an advanced subsonic transport project : final report
- Integrated application of active controls (IAAC) technology to an advanced subsonic transport project : program review
- Integrated application of active controls (IAAC) technology to an advanced subsonic transport project : test ACT system description
- Integrated application of active controls (IAAC) technology to an advanced subsonic transport project : wing planform study and final configuration selection, summary report
- Integrated application of active controls (IACC) technology to an advanced subsonic transport : project plan
- Integrated application of active controls (IACC) technology to an advanced subsonic transport project : current and advanced act control system definition study, summary report
- Integrated application of active controls (IACC) technology to an advanced subsonic transport project : final act configuration evaluation
- Integrated application of active controls (IACC) technology to an advanced subsonic transport project : longitudinal handling qualities study of a relaxed-stability airplane h microform
- 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 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 front method for generating unstructured grid : progress report for the period ended May 31, 1991
- Investigation of installation effects on single-engine convergent-divergent nozzles
- Investigation of radiative interactions in supersonic internal flows : progress report for the period ended May 31, 1991
- Investigation of the asymmetric aerodynamic characteristics of cylindrical bodies of revolution with variations in nose geometry and rotational orientation at angles of attack to 58ånd Mach numbers to 2
- Investigation to advance prediction techniques of the low-speed aerodynamics of V/STOL aircraft
- Inviscid instability of streamwise corner flow
- JBFA--buoyant flight
- Jet-induced ground effects on a parametric flat-plate model in hover
- Kasprzyk airfoil : the first wind-tunnel tests
- Kinematics, influence functions and field quantities for disturbance propagation from moving disturbance sources
- 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
- Laser velocimeter measurements of the flowfield generated by an advanced counterrotating propeller
- Leading-edge deflection optimization for a highly swept arrow-wing configuration
- LinAir:a multi-element discrete vortex Weissinger aerodynamic prediction method
- Literature search of publications concerning the prediction of dynamic inlet flow distortion and related topics
- Losses in channels with increased external turbulence
- Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers
- 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 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
- Mathematical analysis study for radar data processing and enhancement
- Mean velocity, turbulence intensity, and scale in a subsonic turbulent jet impinging normal to a large flat plate
- Measured and predicted aerodynamic coefficients and shock shapes for Aeroassist Flight Experiment (AFE) configuration
- Methodology for matching experimental and computational aerodynamic data
- Methods of applied dynamics
- Micro-optical distributed sensors for aero propulsion applications
- Micro-optical distributed sensors for aero propulsion applications
- Microstructure and orientation effects on properties of discontinuous silicon carbide/aluminum composites
- Mixing noise reduction for rectangular supersonic jets by nozzle shaping and induced screech mixing
- Modifications to the nozzle test chamber to extend nozzle static-test capability
- Multiaxis thrust vectoring using axisymmetric nozzles and postexit vanes on an F/A-18 configuration vehicle
- NASA low-speed centrifugal compressor for 3-D viscous code assessment and fundamental flow physics research
- Nacelle Aerodynamic and Inertial Loads project : test report
- Nacelle aerodynamic and inertial loads (NAIL) project final technical report : energy efficient transport program
- Natural laminar flow experiments on modern airplane surfaces
- Navier-Stokes calculations of scramjet-nozzle-afterbody flowfields
- Navier-Stokes simulation of wind-tunnel flow using LU-ADI factorization algorithm
- 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 problems in flight dynamics involving aerodynamic bifurcations
- Numerical analysis and FORTRAN program for the computation of the turbulent wakes of turbomachinery rotor blades, isolated airfoils and cascade of airfoils
- Numerical approach for the aerodynamic analysis of airfoils with laminar separation
- Numerical computation of complex multi-body compressible Navier-Stokes flows with applications for the integrated space shuttle vehicle
- Numerical methods for the simulation of complex multi-body flows with applications for the Integrated Space Shuttle Vehicle
- Numerical simulation of boundary-layer transition
- Numerical simulation of channel flow transition : resolution requirements and structure of the hairpin vortex
- Numerical simulation of transonic propeller flow using a three-dimensional small disturbance code employing novel helical coordinates
- On minimizing the number of calculations in design-by-analysis codes
- 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 interaction of Gortler vortices and Tollmien-Schlichting waves in curved channel flows at finite Reynolds numbers
- 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 analysis of the NASA/MCAIR 279-3 : an advanced supersonic V/STOL fighter/attack aircraft
- PAN AIR, a computer program for predicting subsonic or supersonic linear potential flows about arbitrary configurations using a higher order panel method
- 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
- Passive control of wing/store flutter
- Performance with and with inlet radial distortion of a transonic fan stage designed for reduced loading in the tip region
- Piloted simulation study of an ILS approach of a twin-pusher business/commuter turboprop aircraft configuration
- Prediction method for two-dimensional aerodynamic losses of cooled vanes using integral boundary-layer parameters
- Prediction of static aerodynamic characteristics for slender bodies alone and with lifting surfaces to very high angles of attack
- Prediction of vortex shedding from circular and noncircular bodies in subsonic flow
- Predictions if airfoil aerodynamic performance degradation due to icing
- Predictive wall adjustment strategy for two-dimensional flexible walled adaptive wind tunnel : a detailed description of the first one-step method
- Preliminary indications of water film distribution and thickness on an airfoil in a water spray
- Pressure distribution for the wing of the YAV-8B airplane; with and without pylons
- Pressure distributions from subsonic tests of an advanced laminar-flow-control wing with leading- and trailing-edge flaps
- Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70
- Pressure measurements on a thick cambered and twisted 58°, elta wing at high subsonic speeds
- Pressure-sensing performance of upright cylinders in a Mach-10 boundary layer
- Production version of the extended NASA-Langley Vortex Lattice FORTRAN Computer Program
- 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
- Real-time estimation of aerodynamic coefficients by means of an extended Kalman filter
- 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
- Relationships between aerodynamic roughness and land use and land cover in Baltimore, Maryland
- Relationships between aerodynamic roughness and land use and land cover in Baltimore, Maryland
- Relative advantages of thin-layer Navier-Stokes and interactive boundary-layer procedures
- Remarks on the layout of the subsonic free jet wind tunnels
- Research study: organization and development of organized convection in the boundary layer : monthly progress report
- Results of the 1987 NASA/JPL balloon flight solar cell calibration program
- Reynolds number effects on pressure loss and turbulence characteristics of four tube-bundle heat exchangers
- Reynolds stress closure in jet flows using wave models
- Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90[ANG]
- Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90°
- Rotary balance data for a single-engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 ̊to 90 ̊/
- Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊/
- SSME interstage seal research : progress report, contract NAS8-33716
- Saturation and the limit of jet mixing enhancement by single frequency plane wave excitation : experiment and technology
- Second-order accurate nonoscillatory schemes for scalar conservation laws
- Secondary electron emission characteristics of ion-textured copper and high-purity isotropic graphite surfaces
- Selected advanced aerodynamic and active control concepts development : summary report
- 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
- Semiempirical method for prediction of aerodynamic forces and moments on a steadily spinning light airplane
- Sensitivity analysis of dynamic aeroelastic responses in transonic flow
- Side forces on forebodies at high angles of attack and Mach numbers from 0.1 to 0.7 : two tangent ogives, paraboloid and cone
- Simplified, inverse, ejector design tool
- Simulation of unsteady rotational flow over propfan configuration
- Singular finite element methods
- Small-scale experiments in STOVL ground effects
- Some VTOL head-up display drive-law problems and solutions
- Some thoughts concerning large load-carrying vehicles
- Sound propagation studies for a large horizontal axis wind turbine
- Spin-tunnel investigation of a 1/15-scale model of an Australian trainer airplane
- Stability boundaries for systems with frequency-model feedback and complementary filter
- State estimation using parallel extended Kalman filters on nonlinear measurements
- Static aerodynamic characteristics of a winged single-stage-to-orbit vehicle at Mach numbers from 0.3 to 4.63
- Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities
- Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing
- Static internal performance of single-expansion-ramp nozzles with various combinations of internal geometric parameters
- Steady pressure measurements on an aeroelastic research wing (ARW-2)
- Stick and rudder : an explanation of the art of flying
- Structural optimization of rotor blades with integrated dynamics and aerodynamics
- Structural shape optimization in multidisciplinary system synthesis
- Study of an efficient long-range Mach 2.7 supersonic transport configuration concept
- 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-10 engine
- Subsonic investigations of vortex interaction control for enhanced high-alpha aerodynamics of a chine forebody/delta wing configuration
- Subsonic panel method for designing wing surfaces from pressure distribution
- Subsonic/transonic stall flutter investigation of a rotating rig
- Suckdown, fountain lift, and pressures induced on several tandem jet V/STOL configurations
- Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations
- Supersonic flow with feeding of energy
- Swirl, expansion ratio and blockage effects on confined turbulent flow
- Techniques for estimating space station aerodynamic characteristics, July 1, 1989 - August 31, 1992
- Tests of a "D" vented thrust deflecting nozzle behind a simulated turbofan engine
- The Aero-Acoustic Propulsion Laboratory
- The Airship ROMA Disaster in Hampton Roads
- The Encyclopedia of Aerodynamics
- The F2 wind-tunnel at Fauga-Mauzac
- The Laminar Boundary Layer Equations
- The Role of freestream turbulence scale in subsonic flow separation
- The aerodynamic performance of several flow control devices for internal flow systems
- The compressible aerodynamics of rotating blades based on an acoustic formulation
- The dynamics and control of fluctuating pressure loads in the reatachment region of a supersonic free shear layer
- The effect of throat contouring on two-dimensional converging-diverging nozzles at static conditions
- The exact calcuation of quadrupole sources for some incompressible flows
- The incorporation of plotting capability into the "unified subsonic supersonic aerodynamic analysis program", version B / Octavio A. Winter ; prepared for Langley Research Center under contract NAS1-14900
- The influence of roll orientation-dependent aerodynamics on the stability of cruciform missile configurations
- The measurement of disturbance levelsin the Langley Research Center 20-inch Mach 6 tunnel
- The miracle of flight
- The pros and cons of code validation
- The simple science of flight : from insects to jumbo jets
- The streamline era
- Theoretical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack
- Theoretical derivation and calibration technique of a hemispherical-tipped, five-hole probe
- Theoretical investigation of non-equilibrium chemistry and optical radiation in hypersonic flow fields
- Thin-element riblet surface : patent application
- Third-order 2N Runge-Kutta schemes with error control
- Three-dimensional inviscid analysis of radial turbine flow and a limited comparison with experimental data
- Three-dimensional singular points in aerodynamics
- Three-dimensional unsteady viscous flow analysis over airfoil sections
- Thrust-induced effects on subsonic longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration
- Tip aerodynamics from wind tunnel test of semi-span wing
- 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 cryogenic test section for the Göttingen tube facility
- Transonic flow field analysis for wing-fuselage configurations
- Transonic flow solutions using a composite velocity procedure for potential, Euler and his equations
- Trends in computational capabilities for fluid dynamics
- Turbulence characteristics of swirling flowfields
- Turbulence characteristics of swirling flowfields
- Turbulent swirling jets with exitation
- Two-dimensional aerodynamic characteristics of an airfoil designed for rotorcraft application
- Two-dimensional aerodynamic characteristics of three rotorcraft airfoils at mach numbers from 0.35 to 0.90
- Ultra high bypass nacelle areodynamics : inlet flow-through high angle of attack distortion test
- Understanding flight
- Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise
- Unsteady aerodynamic simulations of multiple bodies in relative motion : a prototype method
- Unsteady pressure and structural response measurements of an elastic supercritical wing
- Unsteady supersonic aerodynamic theory for interfacing surfaces by the method of potential gradient
- Unstructured and adaptive mesh algorithms for aerodynamic calculations
- Unstructured-grid methods development, lessons learned
- Use of constrained optimization in the conceptual design of a medium-range subsonic transport
- 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
- User's manual for coordinate generation code "CRDSRA"
- VORCOR : a computer program for calculating characteristics of wings with edge vortex separation by using a vortex filament and core model
- Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimization
- Validation of a pair of computer codes for estimation and optimization of subsonic aerodynamic performance of simple hinged-flap systems for thin swept wings
- Verification of performance results for a low-speed 15% eliptical circulation control airfoil
- Vortex breakdown and control experiments in the Ames-Dryden water tunnel
- Vortex methods for separated flows
- Water tunnel flow visualization study through poststall of 12 novel planform shapes
- Wave drag and high-speed performance of supersonic STOVL fighter configurations
- Weak-wave analysis of shock ineraction with a slipstream
- What makes airplanes fly? : history, science, and applications of aerodynamics
- Wind shear hazard definition for a wide body jet
- Wind tunnel aerodynamic characteristics of a transport-type airfoil in a simulated heavy rain environment
- Wind tunnel and analytical investigation of over-the-wing propulsion/air frame interferences for a short-haul aircraft at Mach numbers from 0.6 to 0.78
- Wind tunnel investigations of forebody strakes for yaw control on F/A-18 model at subsonic and transonic speeds
- Wind tunnel results of advanced high speed propellers in the takeoff, climb, and landing operating regimes
- Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊/
- Wind-tunnel investigation of an advanced general aviation canard configuration
- Wind-tunnel investigation of an armed mini remotely piloted vehicle
- Wind-tunnel study of wind loading on a compliant offshore platform
- X-15 Diary
- X-29 flight control system : lessons learned
- X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results
- Your flight questions answered

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