Application Of Generalized Newtonian Theory To Three Dimensional Sharp Nose Shock Detached Bodies At Mach 6 For Angles Of Attack Up To 250

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Application Of Generalized Newtonian Theory To Three Dimensional Sharp Nose Shock Detached Bodies At Mach 6 For Angles Of Attack Up To 250

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Author : George C. Ashby
language : en
Publisher:
Release Date : 1965

Application Of Generalized Newtonian Theory To Three Dimensional Sharp Nose Shock Detached Bodies At Mach 6 For Angles Of Attack Up To 250 written by George C. Ashby and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aerodynamic load categories.

Nasa Technical Note

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Author :
language : en
Publisher:
Release Date : 1971

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Aeronautics categories.

Compendium Of Nasa Langley Reports On Hypersonic Aerodynamics

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Author : Frances E. Sabo
language : en
Publisher:
Release Date : 1987

Compendium Of Nasa Langley Reports On Hypersonic Aerodynamics written by Frances E. Sabo and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with Aerodynamics, Hypersonic categories.

Monthly Catalog Of United States Government Publications

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Author :
language : en
Publisher:
Release Date : 1965

Monthly Catalog Of United States Government Publications written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Government publications categories.

Experimental Boundary Layer Edge Mach Numbers For Two Space Shuttle Orbiters At Hypersonic Speeds

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Author : George C. Ashby
language : en
Publisher:
Release Date : 1972

Experimental Boundary Layer Edge Mach Numbers For Two Space Shuttle Orbiters At Hypersonic Speeds written by George C. Ashby and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Aerodynamic heating categories.

Pitot-pressure profiles and surface pressure measurements have been obtained at four axial stations along the center lines of space shuttle straight-wing and delta-wing orbiters at angles of attack from 200 to approximately 600 and Mach numbers of 20.3 (helium) and 6.8 (air). The results show that the Mach number at the edge of the boundary layer is best predicted by tangent-cone theory up to shock detachment.--P. [i].

Experimental Pressure Distributions On A 120 Cone At Mach Numbers From 2 96 To 4 63 And Angles Of Attack From 0 To 20

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Author : Robert L. Stallings
language : en
Publisher:
Release Date : 1969

Experimental Pressure Distributions On A 120 Cone At Mach Numbers From 2 96 To 4 63 And Angles Of Attack From 0 To 20 written by Robert L. Stallings and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Aerodynamic load categories.

Journal Of The Royal Aeronautical Society

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Author :
language : en
Publisher:
Release Date : 1965

Journal Of The Royal Aeronautical Society written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aeronautics categories.

A Collection Of Technical Papers

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Author :
language : en
Publisher:
Release Date : 1976

A Collection Of Technical Papers written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Aerodynamics categories.

Center Line Pressure Distributions On Two Dimensional Bodies With Leading Edge Angles Greater Than That For Shock Detachment At Mach Number 6 And Angles Of Attack Up To 25

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Author : Theodore J. Goldberg
language : en
Publisher:
Release Date : 1963

Center Line Pressure Distributions On Two Dimensional Bodies With Leading Edge Angles Greater Than That For Shock Detachment At Mach Number 6 And Angles Of Attack Up To 25 written by Theodore J. Goldberg and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Angle of attack (Aerodynamics) categories.

Application Of Generalized Newtonian Theory To Three Dimensional Sharp Nose Shock Detached Bodies At Mach 6 For Angles Of Attack Up To 25 Degrees

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Author : George C. Jr Ashby
language : en
Publisher:
Release Date : 1965

Application Of Generalized Newtonian Theory To Three Dimensional Sharp Nose Shock Detached Bodies At Mach 6 For Angles Of Attack Up To 25 Degrees written by George C. Jr Ashby and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with categories.