Slender Body Theory Based On Approximate Solution Of The Transonic Flow Equation
DOWNLOAD
Download Slender Body Theory Based On Approximate Solution Of The Transonic Flow Equation PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Slender Body Theory Based On Approximate Solution Of The Transonic Flow Equation book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
Slender Body Theory Based On Approximate Solution Of The Transonic Flow Equation
DOWNLOAD
Author : John R. Spreiter
language : en
Publisher:
Release Date : 1959
Slender Body Theory Based On Approximate Solution Of The Transonic Flow Equation written by John R. Spreiter 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.
Approximate solutions of the nonlinear equations of the small disturbance theory of transonic flow are found for the pressure distribution on pointed slender bodies of revolution for flows with free-stream Mach number 1, and for flows that are either purely subsonic or purely supersonic. These results are obtained by application of a method based on local linearization that was introduced recently in the analysis of similar problems in low-dimensional flows. The theory is developed for bodies of arbitrary shapes, and specific results are given for cone-cylinders and for parabolic-arc bodies at zero angle of attack. All results are compared either with existing theoretical results or with experimental data.
Slender Body Theory Based On Approximate Solution Of The Transonic Flow Equation
DOWNLOAD
Author : John R. Spreiter
language : en
Publisher:
Release Date : 1959
Slender Body Theory Based On Approximate Solution Of The Transonic Flow Equation written by John R. Spreiter 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.
Summary: Approximate solutions of the nonlinear equations of the small disturbance theory of transonic flow are found for the pressure distribution on pointed slender bodies of revolution for flows with free-stream Mach number 1, and for flows that are either purely subsonic or purely supersonic. These results are obtained by application of a method based on local linearization that was introduced recently in the analysis of similar problems in low-dimensional flows. The theory is developed for bodies of arbitrary shapes, and specific results are given for cone-cylinders and for parabolic-arc bodies at zero angle of attack. All results are compared either with existing theoretical results or with experimental data.
Nasa Technical Report
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1961
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 1961 with Aerodynamics categories.
Applied Mechanics
DOWNLOAD
Author : M. Hetenyi
language : en
Publisher: Springer Science & Business Media
Release Date : 2013-11-27
Applied Mechanics written by M. Hetenyi and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2013-11-27 with Science categories.
This volume contains the Proceedings of the Twelfth International Congress of Applied Mechanics, held at Stanford University on August 26 to 31, 1968. The Congress was organized by the International Union of Theoretical and Applied Mechanics; members of the IUTAM Congress Committee and Bureau are listed under Congress Organization. The members of the Stanford Organizing Committee, which was responsible for the detailed organization of the Congress, are also given, as are the names of the sponsors and the industrial and educational organizations that contributed so generously to the financial support of the meeting. Those attending the Congress came from 32 countries and totaled 1337 persons, plus wives and children. A list of the registered participants is included in the volume. The technical sessions of the Congress comprised four General Lectures and 281 contributed papers, the latter being presented in groups of five simultaneous sessions. The final choice of the contributed papers was made on the basis of abstracts by an International Papers Commit tee of IUTAM consülting of G. K. BATCHELOR, E. BECKER, N. J. HOFF, and W. T. KOlTER.
Analytical Study Of Soft Landings On Gas Filled Bags
DOWNLOAD
Author : Jack B. Esgar
language : en
Publisher:
Release Date : 1960
Analytical Study Of Soft Landings On Gas Filled Bags written by Jack B. Esgar and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Gas categories.
Theoretical Pressure Distributions On Wings Of Finite Span At Zero Incidence For Mach Numbers Near 1
DOWNLOAD
Author : Alberta Y. Alksne
language : en
Publisher:
Release Date : 1961
Theoretical Pressure Distributions On Wings Of Finite Span At Zero Incidence For Mach Numbers Near 1 written by Alberta Y. Alksne 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, Transonic categories.
A method employed heretofore by the authors to obtain approximate solutions of the transonic flow equation for plane and axisymmetric flow is extended to give reasonable results for wings of finite span, consistent with the known properties of transonic flows. In this method the partial differential equation appropriate to the study of transonic flow is replaced by a nonlinear ordinary differential equation which can be solved by numerical methods. Asymptotic forms of this differential equation are given for very high and very low aspect ratios and analytic results are obtained for certain special cases. Numerical results, calculated by use of electronic computing machines, are given in the form of pressure distribution and pressure drag for two profile shapes, wedge and circular arc, for wings of rectangular plan form. The range of aspect ratios covered extends effectively from zero to infinity and agreement with the asymptotic results is shown at both limits.
Analytic Methods In Aircraft Aerodynamics
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1970
Analytic Methods In Aircraft Aerodynamics 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 Aerodynamics categories.
Index Of Naca Technical Publications
DOWNLOAD
Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1957
Index Of Naca Technical Publications written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aeronautics categories.
Nasa Technical Memorandum
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1971
Nasa Technical Memorandum 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.
Index To Nasa Technical Publications
DOWNLOAD
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.