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Dynamic Response of a Mach 2.5 Axisymmetric Inlet with Engine Or Cold Pipe and Utilizing 60 Percent Supersonic Internal Area Contraction
Language: en
Pages: 64
Authors: Joseph F. Wasserbauer
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1969 - Publisher:

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Dynamic response of supersonic mixed compression inlet coupled to cold pipe or turbojet engine.
NASA Technical Note
Language: en
Pages: 1016
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1970 - Publisher:

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Scientific and Technical Aerospace Reports
Language: en
Pages: 388
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1969 - Publisher:

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NASA Scientific and Technical Reports
Language: en
Pages: 966
Authors: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Categories: Aeronautics
Type: BOOK - Published: 1970 - Publisher:

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NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing
Language: en
Pages: 956
Authors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Categories: Science
Type: BOOK - Published: 1970 - Publisher:

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