Setting up a Rayleight Scattering Based Flow Measuring System in a Large Nozzle Testing Facility
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American Institute of Aeronautics and Astronautics |
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Velocity and Temperature Measurement in Supersonic Free Jets Using Spectrally Resolved Rayleigh Scattering
American Institute of Aeronautics and Astronautics |
The American Society of Mechanical Engineers |
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
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A Unique Test Facility to Measure Liner Performance with a Summary of Initial Test Results
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
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Density fluctuation measurement in supersonic fully expanded jets using Rayleigh scattering
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
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Aerodynamic Facility with MW-System for Flow Control Based on Localized Plasma Generation
American Institute of Aeronautics and Astronautics |