The Calculation Of Three Dimensional Supersonic Flows Around Spherically Capped Smooth Bodies And Wings Theory And Applications
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The Calculation Of Three Dimensional Supersonic Flows Around Spherically Capped Smooth Bodies And Wings Theory And Applications
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Author : Chong-Wei Chu
language : en
Publisher:
Release Date : 1972
The Calculation Of Three Dimensional Supersonic Flows Around Spherically Capped Smooth Bodies And Wings Theory And Applications written by Chong-Wei Chu and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Aerodynamics, Supersonic categories.
The Calculation Of Three Dimensional Supersonic Flows Around Spherically Capped Smooth Bodies And Wings Manual For Computer Programs
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Author : Chong-Wei Chu
language : en
Publisher:
Release Date : 1972
The Calculation Of Three Dimensional Supersonic Flows Around Spherically Capped Smooth Bodies And Wings Manual For Computer Programs written by Chong-Wei Chu and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Aerodynamics, Supersonic categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1986
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1986 with Aeronautics categories.
Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1975
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 1975 with Aeronautics categories.
A Parametric Study Of Effect Of Forebody Shape On Flow Angularity At Mach 8
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Author : Charles B. Johnson
language : en
Publisher:
Release Date : 1974
A Parametric Study Of Effect Of Forebody Shape On Flow Angularity At Mach 8 written by Charles B. Johnson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aerodynamics, Hypersonic categories.
A Short Static Pressure Probe Design For Supersonic Flow
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Author : Shimer Zane Pinckney
language : en
Publisher:
Release Date : 1975
A Short Static Pressure Probe Design For Supersonic Flow written by Shimer Zane Pinckney and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Aerodynamics, Supersonic categories.
Government Reports Announcements
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Author :
language : en
Publisher:
Release Date : 1973
Government Reports Announcements written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Science categories.
Government Reports Index
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Author :
language : en
Publisher:
Release Date : 1973
Government Reports Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Government publications categories.
Aeronautical Engineering
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Author :
language : en
Publisher:
Release Date : 1974
Aeronautical Engineering written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aeronautics categories.
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
The Calculation Of Three Dimensional Supersonic Flows Around Spherically Capped Smooth Bodies And Wings Volume 1 Theory And Application
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Author :
language : en
Publisher:
Release Date : 1972
The Calculation Of Three Dimensional Supersonic Flows Around Spherically Capped Smooth Bodies And Wings Volume 1 Theory And Application written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with categories.
The report describes the theories, the numerical methods and the computer programs developed for determining the inviscid three- dimensional flow about smooth shapes at supersonic speeds. Volume 1 describes the theoretical and numerical approaches and compares two sample cases with experiment; a blunted 15 deg cone at 20 deg angle of attack in helium at M = 14. 9, and a 70 deg slab delta wing at 15 deg angle of attack in air at M = 9.6. The numerical results are in close agreement with the experimental data.