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Author : Jerry Curtis South
Publisher :
ISBN 13 :
Total Pages : 66 pages
Book Rating : 4.58/5 ( download)
Download or read book Calculation of Axisymmetric Supersonic Flow Past Blunt Bodies with Sonic Corners written by Jerry Curtis South and published by . This book was released on 1968 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jerry C. South
Publisher :
ISBN 13 :
Total Pages : 62 pages
Book Rating : 4.13/5 ( download)
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:
Author : Milton Van Dyke
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.26/5 ( download)
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.
Author : Richard W. Barnwell
Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.57/5 ( download)
Download or read book A Time-dependent Method for Calculating Supersonic Angle-of-attack Flow about Axisymmetric Blunt Bodies with Sharp Shoulders and Smooth Nonaxisymmetric Blunt Bodies written by Richard W. Barnwell and published by . This book was released on 1971 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: A time-dependent numerical method for calculating supersonic flow about blunt bodies at large angles of attack is presented. The axisymmetric bodies with sharp shoulders which are treated are constructed with a generator composed of segments of constant curvature. The nonaxisymmetric bodies have continuous slope and curvature. All flow fields are inviscid and adiabatic and have one plane of symmetry. A modification to the method of characteristics is introduced for use at the shock wave. A two-step finite-difference method of second-order accuracy is used at the body surface and in the region between the shock and body. A new finite-difference technique is introduced for use at sharp sonic shoulders. Comparisons of the results of the present method with experiment and the results of other methods are made for the flow of equilibrium air past the Apollo command module at the trim angle of attack and for perfect gas flow past a spherical cap and a spherically blunted cone at angle of attack. Both the cap and the blunted cone are terminated with sharp shoulders. Results are presented also for perfect gas flow past a prolate spheroid with its major axis normal to the flow.
Author : Richard W. Barnwell
Publisher :
ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.35/5 ( download)
Download or read book A Time-dependent Method for Calculating Supersonic Blunt-body Flow Fields with Sharp Corners and Embedded Shock Waves written by Richard W. Barnwell and published by . This book was released on 1970 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Mamoru Inouye
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.04/5 ( download)
Download or read book A Description of Numerical Methods and Computer Programs for Two-dimensional and Axisymmetric Supersonic Flow Over Blunt-nosed and Flared Bodies written by Mamoru Inouye and published by . This book was released on 1965 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 1282 pages
Book Rating : 4.66/5 ( download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1982 with total page 1282 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.
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Author :
Publisher :
ISBN 13 :
Total Pages : 25 pages
Book Rating : 4.35/5 ( download)
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:
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ISBN 13 :
Total Pages : 758 pages
Book Rating : 4.80/5 ( download)
Download or read book Analytic Methods in Aircraft Aerodynamics written by and published by . This book was released on 1970 with total page 758 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Edwin E. Davenport
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.83/5 ( download)
Download or read book Static Longitudinal Aerodynamic Characteristics of Some Supersonic Decelerator Models at Mach Numbers of 2.30 and 4.63 written by Edwin E. Davenport and published by . This book was released on 1969 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
