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Aerodynamic Applications of Underexpanded Hypersonic Viscous Jets
The New Distributed Computerized Control System of JPL's 25-Ft Space Simulator
AIT Model Development for AOEC Hypersonic Wind Tunnel Tests
Aerothermodynamic Simulation in the UAH Aerophysics Facility Ballistic Range
Flow Characteristics of the NASA-Ames Laminar Flow Supersonic Wind Tunnel for Mach 1.6 Operation
Measurements of Supersonic Wing Tip Vortices
Initial Operation of ASTRC/NCKU Transonic Wind Tunnel
Half Model Testing in the Cologne Cryogenic Tunnel (KKK)
Flow Quality Studies of the NASA Lewis Research Center Icing Research Tunnel
CFD Validation of Real Gas Air Flows over a Blunt Body using Multiple Interferometric Views
Numerical Simulation of a Schlieren System from the Fourier Optics Prespective
ETW Control System: Design and First Results
ETW Shakedown Tests and Preliminary Calibration Results
Diffuser Modification Schemes Investigated for the NASA Ames 11-Ft Transonic Wind Tunnel
Fundamentals of Aero-Optics Phenomena (Invited)
Arc Heater Development at AEDC
Using Experimental Results to Validate Numerical Solutions of Rarefield Flow Problems
CFI-Shadowgraph/Schlieren Photography for Aerodynamic Applications
Effects of a Forward-Swept Front Rotor on the Flowfield of a Counterrotation Propeller
Design of Mach 2.4 Quiet Nozzles for the NASA Langley Supersonic Low-Disturbance Pilot Tunnel
A Rational Technique for Calibrating Hot-Wire Probes in Subsonic to Supersonic Speeds
Next Generation Propulsion Simulation Equipment for Use in Wind Tunnels
CVL Application for Supersonic Wind Tunnel of Blow-Down Type
Measurement of Heating Rates for Earth Entry at 13 kms^-^1
Measurement of Scramjet Thrust in Shock Tunnels
CFD Code Validation- An Instrumentation Perspective
Ground Testing Requirements for 21st-Century Aerospace Education
Acoustic Testing of Very High Bypass Ratio Turbofans Using Turbine Powered Scale Models
A CFD Calibration Study For Automotive Shapes
Boundary-Layer Studies In A 2-D Supersonic Nozzle For Quiet-Tunnel Applications
The Nozzle Acoustic Test Rig; An Acoustic and Aerodynamic Free-Jet Facility
Automated Sonic-Venturi Air Flow Metering System for Air Force Trisonic Gasdynamic Facility
Lift, Drag and Thrust Measurement in a Hypersonic Impulse Facility
Computational Flow Imaging For Planar Laser-Induced Fluorescence Applications (CFI-PLIF)
A Measurement of Freely Oscillating Boby Subject to Aerodynamic Forces
Prospects For A Quiet Hypervelocity Shock-Expansion Tunnel
Experiences with Uncertainty Analysis Application in Wind Tunnel Testing
An Experimental Simulation of Flap Flow on Multielement Airfoils at High Reynolds Number