Effect Of Unit Reynolds Number Nose Bluntness Angle Of Attack And Roughness On Transition On A 5 Half Angle Cone At Mach 8

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Effect of Unit Reynolds Number, Nose Bluntness, Angle of Attack, and Roughness on Transition on a 5° Half-angle Cone at Mach 8
Language: en
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Effect of Unit Reynolds Number, Nose Bluntness, Angle of Attack, and Roughness on Transition on a 5° Half-angle Cone at Mach 8

Authors: P. Calvin Stainback
Categories: Aerodynamics, Hypersonic
Type: BOOK - Published: 1969 - Publisher:

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Effect of Unit Reynolds Number, Nose Bluntness, Angle of Attack, and Roughness on Transition on a 5 Degree Half-angle Cone at Mach 8
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Effect of Unit Reynolds Number, Nose Bluntness, Angle of Attack, and Roughness on Transition on a 5° Half-angle Cone at Mach 8
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Effect of Unit Reynolds Number, Nose Bluntness, Angle of Attack, and Roughness on Transition on a 5° Half-angle Cone at Mach 8

Authors: Calvin P. Stainback
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Type: BOOK - Published: 1969 - Publisher:

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A Selected Listing of NASA Scientific and Technical Reports
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A Selected Listing of NASA Scientific and Technical Reports

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NASA Scientific and Technical Reports
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Authors: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
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