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Terminal-shock and Restart Control of a Mach 2.5, Axisymmetric, Mixed Compression Inlet with 40 Percent Internal Contraction
Language: en
Pages: 24
Authors: Robert J. Baumbick
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1974 - Publisher:

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Results of experimental tests conducted on a supersonic, mixed-compression, axisymmetric inlet are presented. The inlet is designed for operation at Mach 2.5 wi
Scientific and Technical Aerospace Reports
Language: en
Pages: 994
Authors:
Categories: Aeronautics
Type: BOOK - Published: - Publisher:

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Scientific and Technical Aerospace Reports
Language: en
Pages: 684
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1974 - Publisher:

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Mach 2.5 Performance of a Bicone Inlet with Internal Focused Compression and 40 Percent Internal Contraction
Language: en
Pages: 68
Authors: David A. Choby
Categories: Aerodynamics
Type: BOOK - Published: 1971 - Publisher:

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Distortion Induced Engine Instability
Language: en
Pages: 194
Authors: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Categories: Aerodynamics
Type: BOOK - Published: 1974 - Publisher:

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