Finite Volume Numerical Methods for Aeroheating Rate Calculations from Infrared Thermographic Data
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American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
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Boundary Layer Transition on Slender Cones in Conventional and Low Disturbance Mach 6wind Tunnels.
American Institute of Aeronautics and Astronautics |
3
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Comparison of Methods for Determining Boundary Layer Edge Conditions for Transition Correlations
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |