Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Hypersonic Strong Interaction Similarity Solutions For Flow Past A Very Slender Axisymetric Body
Download Hypersonic Strong Interaction Similarity Solutions For Flow Past A Very Slender Axisymetric Body full books in PDF, epub, and Kindle. Read online Hypersonic Strong Interaction Similarity Solutions For Flow Past A Very Slender Axisymetric Body ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Hypersonic Strong Interaction Similarity Solutions For Flow Past a Very Slender Axisymmetric Body by : Rand Corporation
Download or read book Hypersonic Strong Interaction Similarity Solutions For Flow Past a Very Slender Axisymmetric Body written by Rand Corporation and published by . This book was released on 1966 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic Strong Interaction Similarity Solutions for Flow Past and Very Slender Axisymmetric Body by : W. B. Bush
Download or read book Hypersonic Strong Interaction Similarity Solutions for Flow Past and Very Slender Axisymmetric Body written by W. B. Bush and published by . This book was released on 1968 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Navier-Stokes hypersonic strong-interaction theory is presented for the flow of a viscous, heat-conducting, compressible fluid past a very slender axisymmetric body, when the ratio of the radius of the body to the radial thickness of the viscous layer(s) (which the body produces and supports), goes to zero. The self-similar leading approximations for the behavior of the flow in these four regions are analyzed, and it is found that an arbitrary body supports '3/4-power' viscous and shock layers. (Author).
Book Synopsis Hypersonic Strong Interaction Similarity Solutions for Flow Past a Very Slender Axisymetric Body by : William B. Bush
Download or read book Hypersonic Strong Interaction Similarity Solutions for Flow Past a Very Slender Axisymetric Body written by William B. Bush and published by . This book was released on 1968 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic Weak-interaction Solutions for Flow Past a Very Slender Axisymmetric Body by : Arthur Kent Cross
Download or read book Hypersonic Weak-interaction Solutions for Flow Past a Very Slender Axisymmetric Body written by Arthur Kent Cross and published by . This book was released on 1971 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic Weak-interaction Solutions for Flow Past a Very Slender Axisymmetric Body by : Arthur K. Cross
Download or read book Hypersonic Weak-interaction Solutions for Flow Past a Very Slender Axisymmetric Body written by Arthur K. Cross and published by . This book was released on 1969 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic Flow Theory by : Wallace Hayes
Download or read book Hypersonic Flow Theory written by Wallace Hayes and published by Elsevier. This book was released on 2012-12-02 with total page 481 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Modern Developments in Gas Dynamics by : W. H. Loh
Download or read book Modern Developments in Gas Dynamics written by W. H. Loh and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 394 pages. Available in PDF, EPUB and Kindle. Book excerpt: During the last decade, the rapid growth of knowledge in the field of fluid mechanics and heat transfer has resulted in many significant ad vances of interest to students, engineers, and scientists. Accordingly, a course entitled "Modern Developments in Fluid Mechanics and Heat Transfer" was given at the University of California to present significant recent theoretical and experimental work. The course consisted of seven parts: I-Introduction; II-Hydraulic Analogy for Gas Dynamics; 111- Turbulence and Unsteady Gas Dynamics; IV-Rarefied and Radiation Gas Dynamics; V-Biological Fluid Mechanics; VI-Hypersonic and Plasma Gas Dynamics; and VII-Heat Transfer in Hypersonic Flows. The material, presented by the undersigned as course instructor and by various guest lecturers, could easily be adapted by other universities for use as a text for a one-semester senior or graduate course on the subject. Due to the extensive notes developed during the University of California course, it was decided to publish the material in three volumes, of which the present is the first. The succeeding volumes will be entitled "Selected Topics in Fluid and Bio-Fluid Mechanics" and "Introduction to Steady and Unsteady Gas Dynamics." Finally, I must express a word of appreciation to my wife Irene and to my children, Wellington Jr. and Victoria, who made it possible for me to write and edit this book in the very quiet atmosphere of our home.
Book Synopsis A Pressure-interaction Theory for Axisymmetric, Hypersonic, Laminar, Unseparated Flows by : John W. Ellinwood
Download or read book A Pressure-interaction Theory for Axisymmetric, Hypersonic, Laminar, Unseparated Flows written by John W. Ellinwood and published by . This book was released on 1970 with total page 65 pages. Available in PDF, EPUB and Kindle. Book excerpt: Theories for axisymmetric viscous interaction are extended to include arbitrary values of the ratios of both surface to free-stream pressure and boundary-layer to body thickness, by identification of a new measure of transverse curvature in the boundary layer. Methods for four limit flows are isolated. Two of the methods are existing solutions for cones with either a strong shock wave or very thin boundary layer. One is a new local solution for general, very thin bodies; it becomes exact when the pressure ratio approaches one or is unbounded. The fourth is a local similarity solution for power-law bodies with linearizable small-disturbance flow; it becomes exact when the ratio of boundary-layer to body thickness vanishes or is unbounded. These methods have provided interpolated estimates of pressure on a very slender cone-cylinder in hypersonic flow that compare well with original experimental data. Similar predictions of heat transfer rate compare poorly. (Author).
Book Synopsis Hypersonic Viscous Interaction Theory for Slender Axisymmetric Bodies by : Harold Mirels
Download or read book Hypersonic Viscous Interaction Theory for Slender Axisymmetric Bodies written by Harold Mirels and published by . This book was released on 1967 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: Effects of viscous interaction are investigated for hypersonic flow over slender axisymmetric bodies. The entire range of interaction, from weak to strong, is considered for nose bluntness not greater than a 3/4 power law. Extensive numerical results are given for the self-similar flow over a 3/4 power law body. These results are correlated and used in a local similarity procedure for finding viscous interaction over arbitrary body shapes. Analytical expressions are derived for weak interaction on a cone and strong interaction on power law bodies. Following Dewey's approach, the local similarity procedure is simplified to a series of algebraic equations. These are solved for flow of air over a cone. Numerical results are presented for cone surface pressure, shear, heat transfer, drag and displacement thickness in all interaction regimes. The drag is in good average agreement with available experimental cone drag data. The analytical development is a unified treatment of viscous interaction effects on two-dimensional as well as axisymmetric bodies. Numerical results for wedges are included. (Author).
Book Synopsis Similar Solutions for Viscous Hypersonic Flow Over a Slender Three-fourths-power Body of Revolution by :
Download or read book Similar Solutions for Viscous Hypersonic Flow Over a Slender Three-fourths-power Body of Revolution written by and published by . This book was released on 1987 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure-Interaction Methods for Axisymmetric, Hypersonic, Laminar, Unseparated Flows by : John W. Ellinwood
Download or read book Pressure-Interaction Methods for Axisymmetric, Hypersonic, Laminar, Unseparated Flows written by John W. Ellinwood and published by . This book was released on 1971 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Local-similarity methods suitable for flows with axisymmetric hypersonic viscous interaction are provided for three limit flows. The first method is for flow with a strong shock wave over sharp or hollow cylinders; this compares with an existing solution for cones and 3/4 power-law bodies. The second is a new local solution for general, very thin bodies; it becomes exact when the pressure ratio approaches 1 or is unbounded. The third, for power-law bodies with linearized inviscid flow, becomes exact when the ratio of boundary-layer to body thickness vanishes or is unbounded. Together with classical results for very thin boundary layers, these diverse methods provide interpolated estimates of pressure and heat transfer rate on a very slender cone-cylinder in hypersonic flow that compare well with original experimental data. (Author).
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1991 with total page 1460 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Download or read book Memorandum written by and published by . This book was released on 1961 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Second-order Small-disturbance Solutions for Hypersonic Flow Over Power-law Bodies by : James Courtland Townsend
Download or read book Second-order Small-disturbance Solutions for Hypersonic Flow Over Power-law Bodies written by James Courtland Townsend and published by . This book was released on 1975 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic Viscous Interaction on a Slender Body of Revolution with Surface Mass Transfer by : Ting Yi Li
Download or read book Hypersonic Viscous Interaction on a Slender Body of Revolution with Surface Mass Transfer written by Ting Yi Li and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analytical formulation is presented of the problem of hypersonic viscous interaction on a very slender body of revolution with a thick boundary layer and mass transfer. Particular attention is directed to the establishment of the mathematical restrictions necessary to ensure the existence of similar solutions of the laminary boundary-layer equations for this class of problems. Yasuhara's analysis is extended to include surface mass transfer and binary mixture effects. It is shown that when the boundary-layer thickness is of the same order of magnitude as the characteristic body dimension, rigorous similarity is possible only for three-quarter-power-law bodies. This is in agreement with Yasuhara's earlier conclusions. Similar solutions to the boundary-layer growth equations exist when the transverse curvature expression is a function of the similarity variable. The criterion for the existence of similar solutions for the problem of hypersonic viscous interaction is that there must be a definite relationship between body surface shape and surface injection velocity. (Author).
Book Synopsis Effect of Body Perturbations on Hypersonic Flow Over Slender Power Law Bodies by : Harold Mirels
Download or read book Effect of Body Perturbations on Hypersonic Flow Over Slender Power Law Bodies written by Harold Mirels and published by . This book was released on 1959 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic Inviscid Flow by : Wallace D. Hayes
Download or read book Hypersonic Inviscid Flow written by Wallace D. Hayes and published by Courier Corporation. This book was released on 2012-07-13 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
