Dryden Flight Research Facility
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The organization Dryden Flight Research Facility represents an institution, an association, or corporate body that is associated with resources found in Indiana State Library.
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Dryden Flight Research Facility
Resource Information
The organization Dryden Flight Research Facility represents an institution, an association, or corporate body that is associated with resources found in Indiana State Library.
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- Dryden Flight Research Facility
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- (EG-IN)1319254
352 Items by the Organization Dryden Flight Research Facility
2 Items that are about the Organization Dryden Flight Research Facility
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- A Constant altitude flight survey method for mapping atmospheric ambient pressures and systematic radar errors
- A NASA/RAE cooperation in the development of a real-time knowledge-based autopilot
- A comparison of Wortmann airfoil computer-generated lift and drag polars with flight and wind tunnel results
- A comparison of experimental and calculated thin-shell leading-edge buckling due to thermal stress
- A comparison of measured and calculated thermal stresses in a hybrid metal matrix composite spar cap element :
- A comparison of time-optimal interception trajectories for the F-8 and F-15 : final report
- A computational fluid dynamics analysis of the hypersonic flight of Pegasus
- A computational fluid dynamics simulation of the hypersonic flight of the Pegasus (TM) vehicle using an artificial viscosity model and a nonlinear filtering method
- A concept for adaptive performance optimization on commercial transport aircraft
- A conversion of wheatstone bridge to current-loop signal conditioning for strain gages
- A flightpath overshoot flying qualities metric for the landing task
- A general solution to the hidden-line problem
- A knowledge-based flight status monitor for real-time application in digital avionics systems
- A knowledge-based system design/information tool for aircraft flight control systems
- A laboratory study on the phase transition for polar stratospheric cloud particles
- A limited in-flight evaluation of the constant current loop strain measurement method
- A preliminary design and analysis of an advanced heat-rejection system for an extreme altitude advanced variable cycle diesel engine installed in high-altitude advanced research plaftorm
- A preliminary investigation of the drag and ventilation characteristics of livestock haulers
- A preliminary look at techniques used to obtain airdata from flight at high angles of attack
- A proposed Kalman filter algorithm for estimation of unmeasured output variables for an F100 turbofan engine
- A radar data processing and enhancement system
- A review of recent developments in flight test techniques at the Ames Research Center, Dryden Flight Research Facility
- A rule-based system for real-time analysis of control systems
- A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring
- A simulation study of turbofan engine deterioration estimation using Kalman filtering techniques
- A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft
- AFTI/F-16 flight test results and lessons
- Accuracies of Southwell and force/stiffness methods in the prediction of buckling strength of hypersonic aircraft wing tubular panels
- Active control technology experience with the space shuttle in the landing regime
- Aeroelastic control of oblique-wing aircraft
- Aerospace Energy Systems Laboratory : requirements and design approach
- Aircraft flight flutter testing at the NASA Ames-Dryden Flight Research Facility
- Aircraft flight test trajectory control
- Aircraft ground vibration testing at NASA Ames-Dryden Flight Research Facility
- Airdata calibration of a high-performance aircraft for measuring atmospheric wind profiles
- Airloads research study
- An Optimal control approach to pilot/vehicle analysis and the Neal-Smith criteria
- An aircraft model for the AIAA controls design challenge
- An application of adaptive learning to malfunction recovery
- An automated calibration laboratory for flight research instrumentation : requirements and a proposed design approach
- An automated stall-speed warning system
- An engineering approach to the use of expert systems technology in avionics applications
- An in-flight interaction of the X-29A canard and flight control system
- An in-flight investigation of ground effect on a forward-swept wing airplane
- An investigation of the cause of failure of flexible thermal protection materials in an aerodynamic environment
- An overview of an experimental demonstration aerotow program
- Analysis of structural response data using discrete modal filters
- Analysis procedures and subjective flights results of a simulator validation and cue fidelity experiment
- Analytic redundancy management mechanization and flight data analysis for the F-8 digital fly-by-wire aircraft flight control sensors
- Application and flight test of linearizing transformations using measurement feedback to the nonlinear control problem
- Application of a flush airdata sensing system to a wing leading edge (LE-FADS)
- Application of a sensitivity analysis technique to high-order digtital flight control systems
- Application of flight systems methodologies to the validation of knowledge-based systems
- Application of fracture mechanics and half-cycle method to the prediction of fatigue life of B-52 aircraft pylon components
- Application of frequency domain handling qualities criteria to the longitudinal landing task
- Application of parameter estimation to highly unstable aircraft
- Archive data base and handling system for the Orbiter flying qualities experiment program
- Augmentor performance of an F100 engine model derivative engine in an F-15 airplane
- Automated flight test management system
- Automation tools for demonstration of goal directed and self-repairing flight control systems
- Autonomous RPRV navigation guidance and control
- Autonomous aircraft initiative study
- Buckling behavior of René 41 tubular panels for a hypersonic aircraft wing
- Buffet induced structural/flight-control system interaction of the X-29A aircraft
- Challenges in modeling the X-29A flight test performance
- Closing the design loop on HiMAT (highly maneuverable aircraft technology)
- Coherent lidar turbulence measurement for gust load alleviation
- Combining and connecting linear, multi-input, multi-output subsystem models
- Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack
- Comparison of flight-measured and calculated temperatures on the space shuttle orbiter
- Comparison of measured and calculated temperatures for a Mach 8 hypersonic wing test structure
- Comparison of measured temperatures, thermal stresses and creep residues with predictions on a build-up titanium structure
- Comparison of pilot effective time delay for cockpit controllers used on space shuttle and conventional aircraft
- Comparison of results obtained from flight tests and simulated tests of a digital electronic engine control system on an F-15 airplane
- Comparison of theoretical and flight-measured local flow aerodynamics for a low-aspect-ratio fin
- Compensating for pneumatic distortion in pressure sensing devices
- Concept of a programmable maintenance processor application to multiprocessing systems
- Configuration management issues and objectives for a real-time research flight test support facility
- Constructing "gloved" wings for aerodynamic studies
- Controlling crippled aircraft--with throttles
- Correlation of analytical and experimental hot structure vibration results
- Current flight test experience related to structural divergence of forward-swept wings
- Decoupling control synthesis for an oblique-wing aircraft
- Design and analysis issues of integrated control systems for high-speed civil transports
- Design and flight test of the propulsion controlled aircraft (PCA) flight control system on the NASA F-15 test aircraft
- Design and initial application of the extended aircraft interrogation and display system : multiprocessing ground support equipment for digital flight systems
- Design and integration of an actuated nose strake control system
- Design considerations of manipulator and feel system characteristics in roll tracking
- Design implications from AFTI/F-16 flight test
- Design of an expert-system flight status monitor
- Design, analysis, and control of large transport aircraft utilizing engine thrust as a backup system for the primary flight controls : semi-annual report in support of grant NAG 2-789
- Design, analysis, and control of large transport aircraft utilizing selective engine thrust as a backup system for the primary flight control
- Development and evaluation of a performance modeling flight test approach based on quasi steady-state maneuvers
- Development and testing of a High Stability Engine Control (HISTEC) system
- Development and use of interactive displays in real-time ground support research facilities
- Development and validation of a general purpose linearization program for rigid aircraft models
- Development experience with a simple expert demonstrator for pilot emergency procedures
- Development of a flight test maneuver autopilot for an F-15 aircraft
- Development of a knowledege acquisition tool for an expert system flight status monitor
- Development of a mobile research flight rest support capability
- Development of a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) system
- Development of a real-time aeroperformance analysis technique for the X-29A advanced technology demonstrator
- Development of a sensitivity analysis technique for multiloop flight control
- Development of a temperature-compensated hot-film anemometer system for boundary-layer transition detection of high performance aircraft
- Development of a thermal and structural model for a NASTRAN finite-element analysis of a hypersonic wing test structure
- Development of an interactive real-time graphics system for the display of vehicle space positioning
- Development of methods for predicting large crack growth in elastic-plastic work-hardening materials in fully plastic conditions
- Digital program for calculating static pressure position error
- Digital signal conditioning for flight test instrumentation
- Dynamic stability and handling qualities tests on a highly augmented, unstable airplane
- Dynamics and controls flight testing of the X-29A airplane
- Effect of control logic modifications on airstart performance of F100 engine model derivative engines in an F-15 airplane
- Effect of creep in titanium alloy Ti6Al-4V at elevated temperature on aircraft design and flight test
- Effect of element size on the solution accuracies of finite-element heat transfer and thermal stress analyses of space shuttle orbiter
- Effect of internal convection and internal radiation on the structural temperatures of space shuttle orbiter
- Effect of time delay on flying qualities : an update
- Effects of bleed air extraction on thrust levels of the F404-GE-400 turbofan engine
- Effects of forced and free convections on structural temperatures of shuttle orbiter during reentry flight
- Effects of mass on aircraft sidearm controller characteristics
- Effects of simplifying assumptions on optimal trajectory estimation for a high-performance aircraft
- Effects of update and refresh rates on flight simulation visual displays
- 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
- Eigensystem synthesis for active flutter suppression on an oblique-wing aircraft
- Engine exhaust characteristics evaluation in support of aircraft acoustic testing
- Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows
- Estimating short-period dynamics using an extended Kalman filter
- Estimation of modal parameters using a wavelet-based approach
- Evaluation of HiMAT aircraft landing approach lateral control gearing using simulation and a visual display
- Evaluation of a flow direction probe and a pilot-static probe on the F-14 airplane at high angles of attack and sideslip
- Exhaust-gas pressure and temperature survey of F404-GE-400 turbofan engine
- Experience with Ada on the F-18 High Alpha Research Vehicle Flight Test Program
- Experience with synchronous and asynchronous digital control systems
- Expert systems development and application
- Expert systems for real-time monitoring and fault diagnosis
- Extraction of aerodynamic parameters for aircraft at extreme flight conditions
- F-18 High Alpha Research Vehicle surface pressures : initial in-flight results and correlation with flow visualization and wind-tunnel data
- F-8 refueling boom ground vibration test
- Failure study of composite materials by the Yeh-Stratton criterion
- Fault detection and accommodation testing on an F100 engine in an F-15 airplane
- Flight characteristics of a manned, low-speed, controlled deep stall vehicle
- Flight control system development and flight test experience with the F-111 mission adaptive wing aircraft
- Flight evaluation of an extended engine life mode on an F-15 airplane
- Flight evaluation of the DEEC secondary engine control air-start capability
- Flight investigation of various control inputs intended for parameter estimation
- Flight measured and calculated exhaust jet conditions for an F100 engine in an F-15 airplane
- Flight research and testing
- Flight stability and control and performance results from the Linear Aerospike SR-71 Experiment (LASRE)
- Flight test and analyses of the B-1 structural mode control system at supersonic flight conditions
- Flight test experience and controlled impact of a large, four-engine, remotely piloted airplane
- Flight test experience with pilot-induced-oscillation suppression filters
- Flight test of a resident backup software system
- Flight test techniques for the X-29A aircraft
- Flight testing and simulation of an F-15 airplane using throttles for flight control
- Flight testing the X-36--the test pilot's perspective
- Flight testing the linear aerospike SR-71 experiment (LASRE)
- Flight tests of external modifications used to reduce blunt base drag
- Flight validation of a pulsed smoke flow visualization system
- Flight-testing of the self-repairing flight control system using the F-15 highly integrated digital electronic control flight research facility
- Flow field survey near the rotational plane of an advanced design propeller on a Jetstar airplane
- Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances
- Flow visualization techniques for flight research
- Flutter clearance of the F-14 variable-sweep transition flight experiment airplane, phase I
- Flutter clearance of the F-14A variable-sweep transition flight experiment airplane : phase 2
- Flutter clearance of the Schweizer 1-36 deep-stall sailplane
- Flying qualities and control system characteristics for superaugmented aircraft
- Formulation and implementation of nonstationary adaptive estimation algorithm with applications to air-data reconstruction
- Formulation of a general technique for predicting pneumatic attenuation errors in airborne pressure sensing devices
- From an automated flight-test management system to a flight-test engineer's workstation
- Full flight envelope direct thrust measurement on a supersonic aircraft
- Ground vibration and flight flutter tests of the single-seat F-16XL aircraft with a modified wing
- Ground vibration and flight flutter tests of the single-seat F-16XL aircraft with a modified wing
- Ground vibration test and flutter analysis of air sampling probe
- Ground vibration test results for drones for aerodynamic and structural testing (DAST)/aeroelastic research wing (ARW-1R) aircraft
- Ground vibration test results of a JetStar airplane using impulsive sine excitation
- Ground-effect analysis of a jet transport airplane
- High altitude turbulence for supersonic cruise vehicles
- High-angle-of-attack pneumatic lag and upwash corrections for a hemispherical flow direction sensor
- High-speed civil transport flight- and propulsion-control technological issues
- High-speed civil transport issues and technology program
- Higher harmonic control analysis for vibration reduction of helicopter rotor systems
- Highly integrated digital electronic control, digital flight control, aircraft model identification and adaptive engine control
- Highly integrated digital engine control system on an NASA F-15 airplane
- Highly maneuverable aircraft technology (HiMAT) flight-flutter test program
- Hypersonic Research Vehicle (HRV) real-time flight test support feasibility and requirements study, Part I, Real-time flight experiment support
- Hypersonic Research Vehicle (HRV) real-time flight test support feasibility and requirements study, part II, Remote computation support for flight systems functions
- Identification of unsteady aerodynamics and aeroelastic integro-differential systems
- Impacts of space shuttle thermal protection system tile on an F-15 aircraft vertical tail
- Implementation of a block Lanczos algorithm for eigenproblem solution of gyroscopic systems
- In-flight evaluation of aerodynamic predictions of an air-launched space booster
- In-flight evaluation of pure time delays in pitch and roll
- In-flight flow visualization with pressure measurements at low speeds on the NASA F-18 high alpha research vehicle
- In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows : design and development
- In-flight load testing of advanced shuttle thermal protection systems
- In-flight rain damage tests of the shuttle thermal protection system
- In-flight transition measurement on a 100
- Inelastic strain analogy for p1ecewise linear computation of creep residues in built-up structures
- Initial flight qualification and operational maintenance of X-29A flight software
- Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance
- Initial flight test of a ground deployed system for flying qualities assessment
- Integrated flight-propulsion control concepts for supersonic transport airplanes
- Investigation of empennage buffeting
- Investigation of seismicity and related effects at NASA Ames-Dryden Flight Research Facility, computer center, Edwards, California
- Laminar flow control : 1981 research and technology studies : presentations made at the Oral Status Review of the NASA Aircraft Energy Efficiency (ACEE) Laminar Flow Control (LFC) Program held at Dryden Flight Research Center, Edwards, California, September 17-18, 1981
- Lee waves : benign and malignant
- Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivaties for the X-29A aircraft
- Low cost tooling material and process for graphite and kevlar composites
- Mach number and flow-field calibration at the advanced design propeller location on the JetStar airplane
- Manual for GetData version 3.1 : a FORTRAN utility program for time history
- Mathematical analysis study for radar data processing and enhancement
- Measured and predicted pressure distributions on the AFTI/F-111 mission adaptive wing
- Measured and predicted structural behavior of the MiMAT tailored composite wing
- Minimum time and fuel flight profiles for an F-15 airplane with a highly integrated digital electronic control system
- Model authoring system for fail safe analysis
- Model reduction for control system design
- Model reduction methods for control design
- Model-following control for an oblique-wing aircraft
- Modeling, simulation, and flight characteristics of an aircraft designed to fly at 100,000 feet
- Modified U.S. Army U-8F ground vibration test
- Monitoring techniques for the X-29A aircraft's high-speed rotating power takeoff shaft
- More than you may want to know about maximum likelihood estimation
- Multiaxis thrust vectoring using axisymmetric nozzles and postexit vanes on an F/A-18 configuration vehicle
- NASA B-57B severe storms flight program
- NASTRAN/FLEXSTAB procedure for static aeroelastic analysis
- National remote computational flight research facility
- Nonlinear maneuver autopilot for the F-15 aircraft
- On-line range prediction system (II)
- On-line robust modal stability prediction using wavelet processing
- Operational and research aspects of a radio-controlled model flight test program
- Operational viewpoint of the X-29A digital flight control system
- Optimal cooperative control synthesis applied to a control-configured aircraft
- Orbiter flying qualities (OFQ) workstation user's guide
- Output model-following control synthesis for an oblique-wing aircraft
- Overview of supersonic laminar flow control research on the F-16XL ships 1 and 2
- Overview of the NASA Ames-Dryden integrated test facility
- Overview of the NASA Dryden Flight Research Facility aeronautical flight projects
- PEst version 2.1 user's manual
- Performance improvements of a highly integrated digital electronic control system for an F-15 airplane
- Performance improvements of an F-15 airplane with an integrated engine-flight control system
- Piloted simulation study of a balloon-assisted deployment of an aircraft at high altitude
- Postflight aerothermodynamic analysis of Pegasus[copyright] using computational fluid dynamic techniques
- Predicted performance benefits of an adaptive digital engine control system on an F-15 airplane
- Predicted pitching moment of an X29A aircraft
- Prediction of service life of aircraft structural components using the half-cycle method
- Preflight transient dynamic analyses of B-52 aircraft carrying space shuttle solid rocket booster drop-test vehicle
- Preliminary airborne measurements for the SR-71 sonic boom propagation experiment
- Preliminary analysis for a Mach 8 crossflow transition experiment on the Pegasus space booster
- Preliminary design of an intermittent smoke flow visualization system
- Preliminary development of an intelligent computer assistant for engine monitoring
- Preliminary experience with a stereoscopic video system in a remotely piloted aircraft application
- Preliminary flight assessment of the X-29A advanced technology demonstrator
- Preliminary flight evaluation of F100 engine model derivative airstart capability in an F-15 airplane
- Preliminary flight test results of the F100 EMD engine in an F-15 airplane
- Preliminary flight-determined subsonic lift and drag characteristics of the X-29A forward-swept-wing airplane
- Preliminary in-flight boundary layer transition measurements on a 45-degree swept wing at Mach numbers between 0.9 and 1.8
- Preliminary results from a subsonic high angle-of-attack flush airdata sensing (HI-FADS) system : design, calibration, and flight test evaluation
- Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flights
- Program for an improved hypersonic temperature-sensing probe
- Project management techniques for highly integrated programs
- Propulsion control experience used in the highly integrated digital electronic control (HIDEC) program
- Qualification needs for advanced integrated aircraft
- Rapid prototyping facility for flight research in artificial-intelligence-based flight systems concepts
- Real-time application of advanced three-dimensional graphic techniques for research aircraft simulation
- Real-time flight test data distribution and display
- Real-time flutter analysis
- Real-time flutter identification
- Real-time in-flight engine performance and health monitoring techniques for flight research application
- Real-time pilot guidance system for improved flight test maneuvers
- Reconfigurable control design for the full X-33 flight envelope
- Remote control of an impact demonstration vehicle
- Research engineering annual report
- Research flight-control system development for the F-18 high alpha research vehicle
- Role of research aircraft in technology development
- Rotor systems research aircraft airplane configuration flight-test results
- Rule-based air combat simulation
- SPF/DB primary structure for supersonic aircraft (T-38 horizontal stabilizer)
- STARS : an integrated general-purpose finite element structural, aeroelastic, and aeroservoelastic analysis computer program
- STARS : an integrated general-purpose finite element structural, aeroelastic, and aeroservoelastic analysis computer program
- Simulation at Dryden Flight Research Facility from 1957 to 1982
- Simulation studies of alternate longitudinal control systems for the space shuttle orbiter in the landing regime
- Simulator evaluation of a remotely piloted vehicle lateral landing task using a visual display
- Simultaneous measurement of temperature and strain using four connecting wires
- Single-strain-gage force/stiffness buckling prediction techniques on a hat-stiffened panel
- Software control and system configuration management : a systems-wide approach
- Space shuttle flying qualities and criteria assessment study--phase 11
- Space shuttle flying qualities criteria assessment phase IV : data acquisition and analysis
- Space shuttle pilot-induced-oscillation research testing
- Spectral contents readout of birefringent sensor
- Spectral contents readout of birefringent sensors
- Strain gage measurement errors in the transient heating of structural components
- Stratospheric turbulence measurements and models for aerospace plane design
- Stress analysis of B-52 pylon hooks
- Stress concentration around a small circular hole in the HiMAT composite plate
- Stress concentration around circular hole in a composite material specimen representative of the X-29A forward-swept wing aircraft
- Summary of in-flight flow visualization obtained from the NASA high alpha research vehicle
- Summary of results of NASA F-15 flight research program
- Surface flow visualization of separated flows on the forebody of an F-18 aircraft and wind-tunnel model
- System overview of the NASA Dryden Integrated Test Facility
- Techniques for hot structures testing
- Techniques for optimizing human-machine information transfer related to real-time interactive display systems
- Techniques used in the F-14 variable-sweep transition flight experiment
- Temperature effect on stress concentration around circular hole in a composite material specimen representative of X-29A forward-swept wing aircraft
- Test and evaluation of the HIDEC engine uptrim algorithm
- Test experience on an ultrareliable computer communication network
- The Aerospace Energy Systems Laboratory : hardware and software implementation
- The F-18 High Alpha Research Vehicle : a high-angle-of-attack testbed aircraft
- The NASA integrated test facility and its impact on flight research
- The PC/AT compatible computer as a mission control center display processor at Ames-Dryden Flight Research Facility
- The Use of an automated flight test management system in the development of a rapid prototyping flight research facility
- The constant current loop : a new paradigm for resistance signal conditioning
- The design and use of a temperature-compensated hot-film anemometer system for boundary-layer flow transition detection on supersonic aircraft
- The development of an airborne information management system for flight test
- The development of an airborne instrumentation computer system for flight test
- The effect of compressor seventh-stage bleed air extraction on performance of the F100-PW-220 afterburning turbofan engine
- The effects of excitation waveforms and shaker moving mass on the measured modal characteristics of a 2- by 5-foot aluminum plate
- The effects of pressure sensor acoustics on airdata derived from a high-angle-of-attack flush airdata sensing (HI-FADS) system
- The implementation and operation of a variable-response electronic throttle control system for a TF-104G aircraft
- The psycology of computer displays in the modern mission control center
- The role of a real-time flight support facility in flight research programs
- The role of simulation in the development and flight test of the HiMAT vehicle
- The role of the Remotely Augmented Vehicle (RAV) laboratory in flight research
- The use of oil for in-flight flow visualization
- The value of early flight evaluation of propulsion concepts using the NASA F-15 research airplane
- The western aeronautical test range of NASA Ames Research Center
- Thermal behavior of a titanium honeycomb-core sandwich panel
- Thermal stress analysis of space orbiter subjected to reentry aerodynamic heating
- Thermal stress analysis of space shuttle orbiter wing skin panel and thermal protection system
- Thermal-fluid analysis of the fill and drain operations of a cryogenic fuel tank
- Thermal-structural panel buckling tests
- Thermal-structural test facilities at NASA Dryden
- Thermoelastic vibration test techniques
- Thermostructural analysis of unconventional wing structures of a Hyper-X hypersonic flight research vehicle for the Mach 7 mission
- Thrust stand evaluation of engine performance improvement algorithms in an F-15 airplane
- Thrust vectoring for lateral-directional stability
- United States atlas of optical telescopes
- User's manual for AeroFcn : a FORTRAN program to compute aerodynamic parameters
- User's manual for EZPLOT version 5.5 : a FORTRAN program for two-dimensional graphic display of data
- Validation of a new flying quality criterion for the landing task
- Validation of the F-18 high alpha research vehicle flight control and avionics systems modifications
- Water tunnel flow visualization study of a 4.4% scale X-31 forebody
- Water tunnel flow visualization using a laser
- Water-tunnel study results of a TF/A-18 and F/A-18 canopy flow visualization
- Wavelet filtering to reduce conservatism in aeroservoelastic robust stability margins
- Western Aeronautical Test Range real-time graphics software package MAGIC
- Wind-tunnel development of an SR-71 aerospike rocket flight test configuration
- Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4
- X-29 flight-research program
- X-29A aircraft structural loads flight testing
- X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results
- X-29A forward-swept-wing flight research program status
- X-33 integrated test facility extended range simulation
- Yeh-Stratton criterion for stress concentrations on fiber-reinforced composite materials
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