Download or read book Supersonic Flow Over Axisymmetric and Non axisymmetric Bodies written by Jefferson Fong and published by . This book was released on 1986 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Supersonic Flow Past a Family of Blunt Axisymmetric Bodies written by Milton Van Dyke and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Some 100 numerical computations have been carried out for unyawed bodies of revolution with detached bow waves. The gas is assumed perfect with y=5/3, 7/5, or 1. Free-stream Mach numbers are taken as 1.2, 1.5, 2, 3, 4, 6, 10, and [infinity symbol]. The results are summarized with emphasis on the sphere and paraboloid.

Download or read book Supersonic Flow Past a Family of Blunt Axisymmetric Bodies written by and published by . This book was released on 1959 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Supersonic Flow Past Family of Blunt Axisymmetric Bodies with List of References written by and published by . This book was released on 1959 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Inviscid Stability of Supersonic Flow Past Heated Or Cooled Axisymmetric Bodies written by Institute for Computer Applications in Science and Engineering and published by . This book was released on 1990 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Supersonic Flow Past a Family of Blunt Axisymmetric Bodies written by Milton Van Dyke and published by . This book was released on 1959 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt: Some 100 numerical computations have been carried out for unyawed bodies of revolution with detached bow waves. The gas is assumed perfect with y=5/3, 7/5, or 1. Free-stream Mach numbers are taken as 1.2, 1.5, 2, 3, 4, 6, 10, and [infinity symbol]. The results are summarized with emphasis on the sphere and paraboloid.

Download or read book An Experimental Investigation of Supersonic Flow Over Axisymmetric Afterbodies with a Centered Propulsive Jet at Angles of Attack written by Johan Agrell and published by . This book was released on 1985 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Numerical Analysis of Supersonic Flow Over an Axisymmetric Body written by P. Kevin Tucker and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Numerical Analysis of Supersonic Flow Over an Axisymmetric Afterbody written by Paul Kevin Tucker and published by . This book was released on 1994 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Stability of the Boundary Layer Formed by Supersonic Flow Past Axisymmetric Bodies written by Stephen James Shaw and published by . This book was released on 1992 with total page 332 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Supersonic Flow Over an Axisymmetric Backward Facing Step written by Eric Loth and published by . This book was released on 1990 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Supersonic Steady and Unsteady Flows Over Slender Axisymmetric Bodies with Continuous Or Discontinuout Surface Slopes written by Jerzy J. Kacprzynski and published by . This book was released on 1965 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report contains the first part of an investigation aimed at finding methods for calculating steady and unsteady inviscid flows past slender three-dimensional bodies of general shape, with continuous or discontinuous slope, but with continuous cross-sectional area. The method is an extension of an approximation proposed by Lighthill (1948) in which the solution is based on the solution of Laplace transformed potential equation and is expressed by Bessel functions. Several characteristic functions, which lead to combinations of Bessel functions, were introduced and calculated. Considered are cases of axial steady flow and cross-flow past a body with discontinuities in slope, as well as unsteady flows for Mach numbers high enough so that it is possible to assume that B squared = (M squared - 1) nearly equal to M squared. The latter investigation induces flows with general unsteady boundary conditions, the body with a harmonically vibrating surface and the gust entry problem. (Author).

Download or read book On the Nature of the Sonic Line for Supersonic and Hypersonic Flow Over Blunt Bodies written by Ronald F. Probstein and published by . This book was released on 1957 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Supersonic Steady and Unsteady Flows Over Slender Axisymmetric Bodies with Continuous Or Discontinuous Surface Slopes written by J. J. Kacprzynski and published by . This book was released on 1965 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Supersonic Steady and Unsteady Flows Over Slender Axisymmetric Bodies with Continuous Or Discontinuous Surface Slopes written by Jerzy J. Kacprzynski and published by . This book was released on 1966 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: The paper contains the second part of an investigation aimed at finding methods for calculating steady and unsteady inviscid flows past slender three-dimensional bodies of general shape, with continuous or discontinuous slope but with continuous cross-sectional area. The report deals with nonlinear flow problems past cones, smooth bodies of arbitrary axisymmetric shape and bodies with discontinuities in slope. The modified method of parametric differentiation is used to solve these problems. Results of numerical calculations are given and compared against results of experiments and results of the method of characteristics. (Author).

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Calculation of Axisymmetric Supersonic Flow Past Blunt Bodies with Sonic Corners Including a Program Description and Listing written by Jerry C. South and published by . This book was released on 1968 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: