Terminal Shock And Restart Control Of A Mach 2 5 Axisymmetric Mixed Compression Inlet With 40 Percent Internal Contraction


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NASA Technical Memorandum


NASA Technical Memorandum

Author:

language: en

Publisher:

Release Date: 1974


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Aeronautical Propulsion


Aeronautical Propulsion

Author:

language: en

Publisher:

Release Date: 1975


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