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Comparison of Wind-tunnel and Flight-measured Base Pressures from the Sharp-leading-edge Upper Vertical Fin of the X-15 Airplane for Turbulent Flow at Mach Numbers from 1.5 to 5.0
Language: en
Pages: 44

Comparison of Wind-tunnel and Flight-measured Base Pressures from the Sharp-leading-edge Upper Vertical Fin of the X-15 Airplane for Turbulent Flow at Mach Numbers from 1.5 to 5.0

Authors: Sheryll Goecke Powers
Categories: Drag (Aerodynamics)
Type: BOOK - Published: 1971 - Publisher:

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NASA Technical Note
Language: en
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NASA Technical Note

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Type: BOOK - Published: 1971 - Publisher:

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Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2
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Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2

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Index of NASA Technical Publications
Language: en
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Authors: United States. National Aeronautics and Space Administration
Categories: Aeronautics
Type: BOOK - Published: 1960 - Publisher:

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A Selected Listing of NASA Scientific and Technical Reports for ...
Language: en
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A Selected Listing of NASA Scientific and Technical Reports for ...

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Type: BOOK - Published: 1954 - Publisher:

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