Synonyme wurden verwendet für:
FLIGHT
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SUPERSONIC
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keywords:(SUPERSONIC FLIGHT)
ASPIRE Aerodynamic Models and Flight Performance
Achieving Global Consensus on Acceptable Sound Levels for Overland Supersonic Flight
ASPIRE Aerodynamic Models and Flight Performance
Achieving Global Consensus on Acceptable Sound Levels for Overland Supersonic Flight
NASAs Quiet Supersonic Aircraft
Review of wave drag reduction techniques: Advances in active, passive, and hybrid flow control
Introduction to the Special Section on the Third AIAA Sonic Boom Prediction Workshop
Background Oriented Schlieren (BOS) of a Supersonic Aircraft in Flight
Recent Enhancements to Modeling Sonic Boom Propagation using Augmented Burgers’ Equation
: A Supersonic Flight Program 1 Payload Design and System Study
Experimental Study of Flight Effects on Slightly Underexpanded Supersonic Jets
Supersonic Flight Dynamics Test 1 - Post-Flight Assessment of Simulation Performance
Effect of Low-Boom Waveform on Focus Boom Using Lossy Nonlinear Tricomi Analysis
Novel approach to dynamic shock attenuation and its validation through computational analysis
Flight Research and Validation Formerly Experimental Capabilities Supersonic Project
Multipoint Aerodynamic Shape Optimization for Subsonic and Supersonic Regimes
Background-Oriented Schlieren Imaging of Supersonic Aircraft in Flight
F-15B 836 Supersonic Research Testbed Capabilities
Supersonic jet and nozzle flows in uniform-flow and free-vortex aerodynamic windows of gas lasers
Toward Improved Predictions of Slender Airframe Aerodynamics Using the F-16XL Aircraft
Planning for Airborne Schlieren Imaging of the X-59 QueSST
Confidence Intervals for Laboratory Sonic Boom Annoyance Tests
NASA Supersonics Research — Leading Toward a Quieter Future!!
Planning for Airborne Schlieren Imaging of the X-59 QueSST
Reduction of Drag Due to Lift at Supersonic Speeds
Simulation and Regression Modeling of NASA’s X-59 Low-Boom Carpets Across America
A Flight Research Overview of WSPR, a Pilot Project for Sonic Boom Community Response
Sonic Boom Testing Performed in NASA Glenn Research Center's 10- by 10-Foot Supersonic Wind Tunnel
Shape of a Supersonic Airplane
Dynamic Characteristics of Combustion Mode Transitions in a Strut-Based Scramjet Combustor Model
The Flight Performance Tests of Supersonic Airplanes
Numerical analysis of internal flow thermal environment in an accelerating high–speed vehicle
LDSD POST2 Modeling Enhancements in Support of SFDT-2 Flight Operations
NASA's Pursuit of Low-Noise Propulsion for Low-Boom Commercial Supersonic Vehicles
NASA's Pursuit of Low-Noise Propulsion for Low-Boom Commercial Supersonic Vehicles
Extension of Multipole Analysis to Laterally Asymmetric Flowfield Around Supersonic Flight Vehicle
Experiments on Discrete Roughness Element Technology for Swept-Wing Laminar Flow Control