Viscous Hypersonic Flow Over Pointed Cones At Low Reynolds Numbers
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Viscous Hypersonic Flow Over Pointed Cones At Low Reynolds Numbers
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Author : H. F. Waldron
language : en
Publisher:
Release Date : 1966
Viscous Hypersonic Flow Over Pointed Cones At Low Reynolds Numbers written by H. F. Waldron and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Aerodynamics, Hypersonic categories.
Viscous Hypersonic Flows Over Pointed Cones At Low Reynolds Numbers
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Author : H. F. Waldron
language : en
Publisher:
Release Date : 1966
Viscous Hypersonic Flows Over Pointed Cones At Low Reynolds Numbers written by H. F. Waldron and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with categories.
An experimental and analytical study of viscous hypersonic flow over pointed cones with particular emphasis on the viscous-layer regime is presented. Shock tunnel measurements of heat transfer to 5, 10 and 20 degree half-angle cones and of pressure on the 20 degree cone are compared with the predictions of a viscous-inviscid interaction analysis (Probstein and Elliot) including transverse curvature, of a viscous-layer nonslender cone analysis (Cheng) and of an extension of the nonslender cone analysis incorporating effects of slenderness. The large rise in heat transfer predicted by the transverse curvature theory is not observed and close agreement is obtained with the nonslender cone viscous-layer predictions. An extension of the nonslender cone analysis is presented where the effects of cone slenderness are included by a perturbation analysis. The solution of the resulting equations reveals that the net effect of transverse curvature and of other effects associated with cone slenderness is small in the viscous-layer regime for not-too-slender cones. Good agreement of the 10 and the 20 degree cone experimental data is obtained with this extension of the nonslender solution. (Author).
Static Pressure On Sharp And Blunt Cones In Conical And Parallel Low Density Flow
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Author : Max Kinslow
language : en
Publisher:
Release Date : 1974
Static Pressure On Sharp And Blunt Cones In Conical And Parallel Low Density Flow written by Max Kinslow and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Cone categories.
The static pressure distribution on sharp and blunt 10-deg half-angle cones was measured under rarefied conditions in both a uniform and a source flow field. Angle of attack of the cones was varied up to 10 deg. Pressure distributions are presented for cold-wall conditions at 18.0 = or
Viscous Hypersonic Flows Over Pointed Cones At Low Reynolds Numbers
DOWNLOAD
Author : H. F. Waldron
language : en
Publisher:
Release Date : 1966
Viscous Hypersonic Flows Over Pointed Cones At Low Reynolds Numbers written by H. F. Waldron and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Aerodynamics, Hypersonic categories.
An experimental and analytical study of viscous hypersonic flow over pointed cones with particular emphasis on the viscous-layer regime is presented. Shock tunnel measurements of heat transfer to 5, 10 and 20 degree half-angle cones and of pressure on the 20 degree cone are compared with the predictions of a viscous-inviscid interaction analysis (Probstein and Elliot) including transverse curvature, of a viscous-layer nonslender cone analysis (Cheng) and of an extension of the nonslender cone analysis incorporating effects of slenderness. The large rise in heat transfer predicted by the transverse curvature theory is not observed and close agreement is obtained with the nonslender cone viscous-layer predictions. An extension of the nonslender cone analysis is presented where the effects of cone slenderness are included by a perturbation analysis. The solution of the resulting equations reveals that the net effect of transverse curvature and of other effects associated with cone slenderness is small in the viscous-layer regime for not-too-slender cones. Good agreement of the 10 and the 20 degree cone experimental data is obtained with this extension of the nonslender solution. (Author).
Shock Wave Shapes And Surface Pressures On Hemisphere And Cone Cylinders In Low Density Hypersonic Flow Including Ablation
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Author : Daryl J. Monson
language : en
Publisher:
Release Date : 1970
Shock Wave Shapes And Surface Pressures On Hemisphere And Cone Cylinders In Low Density Hypersonic Flow Including Ablation written by Daryl J. Monson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Ablation (Aerothermodynamics) categories.
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Study Of High Density Hypervelocity Flows And Similitudes
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Author : Cornell Aeronautical Laboratory
language : en
Publisher:
Release Date : 1967
Study Of High Density Hypervelocity Flows And Similitudes written by Cornell Aeronautical Laboratory and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Gas flow categories.
Propulsion Re Entry Physics
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Author : Michał Lunc
language : en
Publisher: Elsevier
Release Date : 2014-05-09
Propulsion Re Entry Physics written by Michał Lunc and has been published by Elsevier this book supported file pdf, txt, epub, kindle and other format this book has been release on 2014-05-09 with Technology & Engineering categories.
Propulsion Re-Entry Physics deals with the physics of propulsion re-entry and covers topics ranging from inductive magnetoplasmadynamic (MPD) propulsion systems to launch systems and orbiting maneuvering systems. Problems of re-entry aerodynamics are considered, along with interaction problems in hypersonic fluid dynamics. Comprised of 31 chapters, this volume begins with a detailed account of the quasi-steady adiabatic vaporization and subsequent exothermic decomposition of a pure monopropellant spherical droplet in the absence of free and forced convection. The discussion then turns to results of calculations on MPD machines working in the intermittent and in the continuous mode; inductive plasma accelerators with electromagnetic standing waves; and spherical rocket motors for space and upper stage propulsion. Subsequent chapters focus on pulsed plasma satellite control systems; drag and stability of various Mars entry configurations; hypersonic laminar boundary layers around slender bodies; and effects of an entry probe gas envelope on experiments concerning planetary atmospheres. This book will appeal to students, practitioners, and research workers interested in propulsion re-entry and the accompanying physics.
Technical Abstract Bulletin
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Author : Defense Documentation Center (U.S.)
language : en
Publisher:
Release Date : 1964
Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Military art and science categories.
Theoretical Modelling Of Aeroheating On Sharpened Noses Under Rarefied Gas Effects And Nonequilibrium Real Gas Effects
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Author : Zhi-Hui Wang
language : en
Publisher: Springer
Release Date : 2014-08-28
Theoretical Modelling Of Aeroheating On Sharpened Noses Under Rarefied Gas Effects And Nonequilibrium Real Gas Effects written by Zhi-Hui Wang and has been published by Springer this book supported file pdf, txt, epub, kindle and other format this book has been release on 2014-08-28 with Technology & Engineering categories.
Theoretical Modelling of Aeroheating on Sharpened Noses under Rarefied Gas Effects and Nonequilibrium Real Gas Effects employs a theoretical modeling method to study hypersonic flows and aeroheating on sharpened noses under rarefied gas effects and nonequilibrium real gas effects that are beyond the scope of traditional fluid mechanics. It reveals the nonlinear and nonequilibrium features, discusses the corresponding flow and heat transfer mechanisms, and ultimately establishes an analytical engineering theory framework for hypersonic rarefied and chemical nonequilibrium flows. The original analytical findings presented are not only of great academic significance, but also hold considerable potential for applications in engineering practice. The study explores a viable new approach, beyond the heavily relied-upon numerical methods and empirical formulas, to the present research field, which could be regarded as a successful implementation of the idea and methodology of the engineering sciences.
Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1970
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 1970 with Aeronautics categories.