Download or read book Nonlinear Asymptotic Theory of Hypersonic Flow Past a Circular Cone written by Chao-Kang Feng and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Asymptotic Hypersonic Flow Theory for Blunted Slender Cones and Wedges written by John W. Ellinwood and published by . This book was released on 1966 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: Inviscid hypersonic flow over slender, unyawed circular cones and wedges has been perturbed for the effect of nose bluntness far behind the nose. The resulting singular-perturbation problem is solved with matched inner and outer asymptotic expansions. For both plane and axisymmetric flows, the leading perturbation in surface pressure is an eigensolution which varies as the real part of downstream distance raised to complex powers. The imaginary parts of all exponents are multiples of a fundamental frequency, and all harmonics decay at a rate which depends on Mach number, specific heat ratio and body geometry. For blunted wedges, the perturbation equations are integrated in closed form generally. The displacement of the shock asymptote relative to the body asymptote was determined without approximation. For blunted cones, it is shown that logarithms do not appear where the afterbody is specified, unlike the inverse problem of flow behind a hyperboloidal shock. Three limiting axisymmetric cases are considered: infinite Mach number, specific heat ratio of unity, and a combination of these known as the NEWTONIAN SLENDER BODY limit. (Author).

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1974 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 Nonlinear Instability of Hypersonic Flow Past a Wedge written by Institute for Computer Applications in Science and Engineering and published by . This book was released on 1991 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1998 with total page 980 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Angle of Attack and Bluntness on the Hypersonic Flow Over a 15 semiapex Cone in Helium written by Joseph W. Cleary and published by . This book was released on 1970 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Hypersonic Flow Research written by F.R. Riddell and published by Elsevier. This book was released on 2012-12-02 with total page 769 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Download or read book Tables for Supersonic Flow of Helium Around Right Circular Cones at Zero Angle of Attack written by Joseph L. Sims and published by . This book was released on 1973 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of the calculation of supersonic flow of helium about right circular cones at zero angle of attack are presented in tabular form. The calculations were performed using the Taylor-Maccoll theory. Numerical integrations were performed using a Runge-Kutta method for second-order differential equations. Results were obtained for cone angles from 2.5 to 30 degrees in regular increments of 2.5 degrees. In all calculations the desired free-stream Mach number was obtained to five or more significant figures.

Download or read book Hypersonic Flow Past a Slender Elliptic Cone written by Hsiung Ming Lee and published by . This book was released on 1978 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate analytical solution is obtained for hypersonic flow past a slender elliptic cone at small angle of attack. The analysis is based on perturbations of hypersonic flow past a circular cone aligned with the free stream, the perturbations stemming from the linear combination of small angle of attack and small cross-section eccentricity. By means of previously obtained hypersonic approximations for the basic-cone problem, closed-form approximate solutions for the perturbation equations are obtained within the framework of hypersonic small disturbance theory. Results for the shock shape, shock-layer structure, and surface conditions are presented, together with comparisons with experimental data. (Author).

Download or read book Hypersonic Flow Theory Inviscid flows written by Wallace Dean Hayes and published by . This book was released on 1966 with total page 632 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Approximate Analytical Solutions for Hypersonic Flow Over Slender Power Law Bodies written by Harold Mirels and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Download or read book 30th AIAA Fluid Dynamics Conference written by and published by . This book was released on 1999 with total page 560 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Tables for Supersonic Flow Around Right Circular Cones at Zero Angle of Attack written by Joseph L. Sims and published by . This book was released on 1964 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Theoretical and Experimental Study of Hypersonic Flow Over Flared Bodies at Incidence written by John V. Rakich and published by . This book was released on 1966 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Viscous Hypersonic Flow Past a Slender Cone written by V. S. Nikolaev and published by . This book was released on 1967 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Finding Guide to AIAA Meeting Papers written by American Institute of Aeronautics and Astronautics. Technical Information Service and published by . This book was released on 1996 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt: