Calculation Of Axisymmetric Supersonic Flow Past Blunt Bodies With Sonic Corners
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Author | : Jerry Curtis South |
Publisher | : |
Total Pages | : 66 |
Release | : 1968 |
Genre | : Mathematical models |
ISBN | : |
Download Calculation of Axisymmetric Supersonic Flow Past Blunt Bodies with Sonic Corners Book in PDF, Epub and Kindle
Author | : Jerry C. South |
Publisher | : |
Total Pages | : 62 |
Release | : 1968 |
Genre | : |
ISBN | : |
Download Calculation of Axisymmetric Supersonic Flow Past Blunt Bodies with Sonic Corners, Including a Program Description and Listing Book in PDF, Epub and Kindle
Author | : Milton Van Dyke |
Publisher | : |
Total Pages | : 32 |
Release | : 1959 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Supersonic Flow Past a Family of Blunt Axisymmetric Bodies Book in PDF, Epub and Kindle
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 | : |
Total Pages | : 84 |
Release | : 1971 |
Genre | : Finite differences |
ISBN | : |
Download A Time-dependent Method for Calculating Supersonic Angle-of-attack Flow about Axisymmetric Blunt Bodies with Sharp Shoulders and Smooth Nonaxisymmetric Blunt Bodies Book in PDF, Epub and Kindle
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 | : |
Total Pages | : 76 |
Release | : 1970 |
Genre | : Blunt bodies |
ISBN | : |
Download A Time-dependent Method for Calculating Supersonic Blunt-body Flow Fields with Sharp Corners and Embedded Shock Waves Book in PDF, Epub and Kindle
Author | : Mamoru Inouye |
Publisher | : |
Total Pages | : 42 |
Release | : 1965 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download A Description of Numerical Methods and Computer Programs for Two-dimensional and Axisymmetric Supersonic Flow Over Blunt-nosed and Flared Bodies Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1282 |
Release | : 1982 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, Epub and Kindle
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.
Author | : |
Publisher | : |
Total Pages | : 25 |
Release | : 1959 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Supersonic Flow Past Family of Blunt Axisymmetric Bodies [with List of References] Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 758 |
Release | : 1970 |
Genre | : Aerodynamics |
ISBN | : |
Download Analytic Methods in Aircraft Aerodynamics Book in PDF, Epub and Kindle
Author | : Edwin E. Davenport |
Publisher | : |
Total Pages | : 40 |
Release | : 1969 |
Genre | : Acceleration (Mechanics) |
ISBN | : |
Download Static Longitudinal Aerodynamic Characteristics of Some Supersonic Decelerator Models at Mach Numbers of 2.30 and 4.63 Book in PDF, Epub and Kindle