Approximate Analytical Solutions For Hypersonic Flow Over Slender Power Law Bodies
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Approximate Analytical Solutions For Hypersonic Flow Over Slender Power Law Bodies
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Author : Harold Mirels
language : en
Publisher:
Release Date : 1959
Approximate Analytical Solutions For Hypersonic Flow Over Slender Power Law Bodies written by Harold Mirels and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamics, Hypersonic categories.
Approximate analytical solutions are presented for two-dimensional and axisymmetric hypersonic flow over slender power law bodies. Both zero-order (M->∞) and first-order (small but nonvanishing values of 1/(Mδ)2) solutions are presented, where M is free-stream Mach number and δ is a characteristic slope. These solutions are compared with exact numerical integrations of the equations of motion and appear to be accurate particularly when the shock is relatively close to the body.
Approximate Analytical Solutions For Hypersonic Flow Over Slender Power Law Bodies
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Author : Harold Mirels
language : en
Publisher:
Release Date : 1959
Approximate Analytical Solutions For Hypersonic Flow Over Slender Power Law Bodies written by Harold Mirels and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.
Approximate Analytical Solutions For Hypersonic Flow Over Slender Power Law Bodies
DOWNLOAD
Author : Harold Mirels
language : en
Publisher:
Release Date : 1959
Approximate Analytical Solutions For Hypersonic Flow Over Slender Power Law Bodies written by Harold Mirels and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamics, Hypersonic categories.
Nasa Technical Report
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Author :
language : en
Publisher:
Release Date : 1959
Nasa Technical Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamics categories.
Effect Of Body Perturbations On Hypersonic Flow Over Slender Power Law Bodies
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Author : Harold Mirels
language : en
Publisher:
Release Date : 1959
Effect Of Body Perturbations On Hypersonic Flow Over Slender Power Law Bodies written by Harold Mirels and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamics, Hypersonic categories.
Advances In Applied Mechanics
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Author :
language : en
Publisher: Academic Press
Release Date : 1962-01-01
Advances In Applied Mechanics written by and has been published by Academic Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962-01-01 with Technology & Engineering categories.
Advances in Applied Mechanics
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 categories.
On The Similar Solutions Of Strong Blast Waves And Their Application To Steady Hypersonic Flow
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Author : Eric François Brocher
language : en
Publisher:
Release Date : 1961
On The Similar Solutions Of Strong Blast Waves And Their Application To Steady Hypersonic Flow written by Eric François Brocher and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamics, Hypersonic categories.
The exact 'constant-energy' solution of strong blast waves is expanded in powers of the density ratio across the shock wave; physical quantities are expressed directly as functions of the similitude parameter. The range of validity for t.;e application of this solution to hypersonic flow is then studied as a function of the density ratio. The general similar solution of the strong blast wave is found in the Newtonian approximation. The results are applied to power-law bodies in hypersonic flow using the equivalence principle. The pressure distribution on slender bodies of arbitrary shape is obtained and agrees with the Newton-Busemann pressure formula. Higher-order approximations are derived for the cases in which the shock layer is thin. A simple pressure formula is obtained and some of its applications are shown. (Author).
Hypersonic Inviscid Flow
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Author : Wallace D. Hayes
language : en
Publisher: Courier Corporation
Release Date : 2012-07-13
Hypersonic Inviscid Flow written by Wallace D. Hayes and has been published by Courier Corporation this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-07-13 with Science categories.
Unified, self-contained view of nonequilibrium effects, body geometries, and similitudes available in hypersonic flow and thin shock layer; appropriate for graduate-level courses in hypersonic flow theory. 1966 edition.
Index To Nasa Technical Publications
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960
Index To Nasa Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.