eBook File Effects Of Leading Edge Bluntness And Ramp Deflection Angle On Laminar Boundary Layer Separation In Hypersonic Flow PDF

Language: en
Pages: 34

Effects of Leading-edge Bluntness and Ramp Deflection Angle on Laminar Boundary-layer Separation in Hypersonic Flow

Authors: James Courtland Townsend

Categories: Aerodynamics, Hypersonic

Type: BOOK - Published: 1966 - Publisher:

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Language: en
Pages: 128

Effects of Wall Cooling and Leading-edge Blunting on Ramp-induced, Laminar Flow Separations at Mach Numbers from 3 Through 6

Authors: J. Don Gray

Categories: .

Type: BOOK - Published: 1972 - Publisher:

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The effects of wall cooling and nose bluntness on laminar and transitional reattaching flows induced by a 9.5-degree ramp were investigated at Mach numbers from

Language: en
Pages: 536

NASA Technical Note

Authors:

Categories:

Type: BOOK - Published: 1970 - Publisher:

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Language: en
Pages: 562

Scientific and Technical Aerospace Reports

Authors:

Categories: Aeronautics

Type: BOOK - Published: 1991 - Publisher:

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Language: en
Pages: 2084

A Selected Listing of NASA Scientific and Technical Reports for 1966

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

Categories: Aeronautics

Type: BOOK - Published: 1967 - Publisher:

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Effects of Leading-edge Bluntness and Ramp Deflection Angle on Laminar Boundary-layer Separation in Hypersonic Flow

Effects of Wall Cooling and Leading-edge Blunting on Ramp-induced, Laminar Flow Separations at Mach Numbers from 3 Through 6

NASA Technical Note

Scientific and Technical Aerospace Reports

A Selected Listing of NASA Scientific and Technical Reports for 1966