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[American Institute of Aeronautics and Astronautics 9th Applied Aerodynamics Conference - Baltimore,MD,U.S.A. (23 September 1991 - 25 September 1991)] 9th Applied Aerodynamics Conference - Pressure and temperature fluctuations in an axisymmetric flowfield due to shock-boundary layer interactions at high Reynolds numbers at Mach 6

โœ Scribed by FLANAGAN, JR., M.; HAYES, J.


Book ID
121038037
Publisher
American Institute of Aeronautics and Astronautics
Year
1991
Weight
754 KB
Category
Article

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