Hypersonic Inviscid Flow PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Hypersonic Inviscid Flow PDF full book. Access full book title Hypersonic Inviscid Flow.
Author | : Wallace D. Hayes |
Publisher | : Courier Corporation |
Total Pages | : 628 |
Release | : 2012-07-13 |
Genre | : Science |
ISBN | : 0486160483 |
Download Hypersonic Inviscid Flow Book in PDF, ePub and Kindle
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.
Author | : Wallace Hayes |
Publisher | : Elsevier |
Total Pages | : 481 |
Release | : 2012-12-02 |
Genre | : Technology & Engineering |
ISBN | : 032314876X |
Download Hypersonic Flow Theory Book in PDF, ePub and Kindle
Hypersonic Flow Theory presents the fundamentals of fluid mechanics, focusing on the hypersonic flow theory and approaches in theoretical aerodynamics. This book discusses the assumptions underlying hypersonic flow theory, unified supersonic-hypersonic similitude, two-dimensional and axisymmetric bodies, and circular cylinder. The constant-streamtube-area approximation, streamtube-continuity methods, and tangent-wedge and tangent-cone are also deliberated. This text likewise covers the similar laminar boundary layer solutions, bluntness induced interactions on slender bodies, and free molecule transfer theory. The dynamics of hypersonic flight or hypersonic wing theory, magnetohydrodynamic theory, or any developments involving treatment of the Boltzmann equation are not included. This publication is intended for hypersonic aerodynamicists, students, and researchers conducting work on the hypersonic flow phenomena.
Author | : Wallace D. Hayes |
Publisher | : |
Total Pages | : 602 |
Release | : 1966 |
Genre | : |
ISBN | : |
Download Hypersonic flow theory. 1. Inviscid flows Book in PDF, ePub and Kindle
Author | : Wallace Dean Hayes |
Publisher | : |
Total Pages | : 602 |
Release | : 1966 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : 9780123343611 |
Download Hypersonic Flow Theory Book in PDF, ePub and Kindle
Author | : John David Anderson |
Publisher | : AIAA |
Total Pages | : 710 |
Release | : 1989 |
Genre | : Science |
ISBN | : 9781563474590 |
Download Hypersonic and High Temperature Gas Dynamics Book in PDF, ePub and Kindle
This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.
Author | : G. G. Chernyi |
Publisher | : Academic Press |
Total Pages | : 277 |
Release | : 2013-10-22 |
Genre | : Technology & Engineering |
ISBN | : 1483271684 |
Download Introduction to Hypersonic Flow Book in PDF, ePub and Kindle
Introduction to Hypersonic Flow has been made available to the English speaking reader because of its usefulness for those individuals desirous of obtaining an introduction to the subject. Written by an internationally acknowledged expert in the field of hypersonic flow, the book makes available heretofore unpublished Soviet work, as well as published work little known outside the Soviet Union. The author has however made every effort to include, where appropriate. Western references for the work he discusses. Starting with a general introductory chapter on hypersonic aerodynamics and aerodynamic problems, the remainder of the book concentrates on the inviscid, perfect fluid aspects of hypersonic flow, with emphasis on the fundamental concepts and rational methods of calculation. The book is directed to students of aerodynamics and gas dynamics, as well as to scientists and engineers interested in problems of hypersonic flight. The level of approach is such that it should prove particularly useful as an undergraduate and introductory graduate text.
Author | : Jean-Antoine Desideri |
Publisher | : Springer |
Total Pages | : 268 |
Release | : 1992-01-17 |
Genre | : Science |
ISBN | : 9783540544289 |
Download Hypersonic Flows for Reentry Problems Book in PDF, ePub and Kindle
One of the most challenging problems of modern engineering is undoubtedly the prediction of hypersonic flows around space vehicles in reentry conditions. Indeed, the difficulties are numerous: first of all, these flows are very difficult to model, since very complex physical and chemical phenomena take place during the reentry phase; secondly, temperature, velocity and enthalpy are very high and densities are very low, making the reentry process very difficult to reproduce in ground-based experiments. The past three decades have seen important efforts in computational fluid dynam ics relying on the use of supercomputers to simulate these very complicated flows. The numerical simulation based on imperfect models and methods which were es sentially designed for transonic and supersonic flows has still a long way to go in order to be able to predict these hypersonic reentry flows very accurately. This situation has motivated very strong international cooperative efforts with, as the most visible consequences, the EuropelUnited States Short Courses on Hy personics, which were held in Paris, in 1987 [1,2], Colorado Springs in 1989 [3], and Aachen in 1990 [3]. The workshop on Hypersonics whose results are presented and analysed in these volumes is also a direct consequence of this international cooperation. This scien tific event was an initiative of P. Perrier, Head of the Theoretical Aerodynamics Department of DASSAULT AVIATION, who played a key role in the identification of the critical problems and the realisation of experiments, within the Hermes R&D program framework.
Author | : Arnold Polak |
Publisher | : |
Total Pages | : 48 |
Release | : 1970 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download On the Hypersonic Flow Past Blunted, Flat Delta Wings Book in PDF, ePub and Kindle
The flow of a perfect gas over the slab portion of a blunted delta wing flying at hypersonic speeds is studied. A set of approximate equations is derived and a solution - for an inviscid flow - is obtained. Using this solution as a representation for the inviscid flow problem, a formulation to the laminar boundary-layer equations is presented; one which is applicable to the flow field's azimuthal planes where the crossflow gradients are not too large. Numerical solutions to these boundary-layer equations have been obtained; however, these are restricted to the azimuthal planes and near to the leading edges. The results indicate the presence of a dividing surface streamline since a numerical solution could not be obtained near the centerplane of the wing, where the crossflow velocity is large. (Author).
Author | : William L. Gose |
Publisher | : |
Total Pages | : 164 |
Release | : 1971 |
Genre | : Inviscid flow |
ISBN | : |
Download A Thin-shock-layer Solution for Nonequilibrium, Inviscid Hypersonic Flows in Earth, Martian, and Venusian Atmospheres Book in PDF, ePub and Kindle
An approximate inverse solution is presented for the nonequilibrium flow in the inviscid shock layer about a vehicle in hypersonic flight. The method is based upon a thin-shock-layer approximation and has the advantage of being applicable to both subsonic and supersonic regions of the shock layer. The relative simplicity of the method makes it ideally suited for programming on a digital computer with a significant reduction in storage capacity and computing time required by other more exact methods. Comparison of nonequilibrium solutions for an air mixture obtained by the present method is made with solutions obtained by two other methods. Additional cases are presented for entry of spherical nose cones into representative Venusian and Martian atmospheres. A digital computer program written in FORTRAN language is presented that permits an arbitrary gas mixture to be employed in the solution. The effects of vibration, dissociation, recombination, electronic excitation, and ionization are included in the program.
Author | : F.R. Riddell |
Publisher | : Elsevier |
Total Pages | : 769 |
Release | : 2012-12-02 |
Genre | : Transportation |
ISBN | : 0323142621 |
Download Hypersonic Flow Research Book in PDF, ePub and Kindle
Progress in Astronautics and Rocketry, Volume 7: Hypersonic Flow Research compiles papers presented at a conference on hypersonics held at the Massachusetts Institute of Technology in August 1961. This book discusses the low Reynolds number effects, chemical kinetics effects, inviscid flow calculations, and experimental techniques relating to the problems in acquiring an understanding of hypersonic flow. The structure and composition of hypersonic wakes with attendant complex chemical kinetic effects is only briefly mentioned. This text consists of five parts. Parts A to C comprise of theoretical papers on the problems of calculating flow fields at hypersonic speeds. The experimental techniques that are of immediate practical interest in view of the difficulty of flight testing are discussed in Parts D and E. This publication is beneficial to engineers involved in advanced design problems.