The Inviscid Stability Of Supersonic Flow Past Heated Or Cooled Axisymmetric Bodies
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Author | : Institute for Computer Applications in Science and Engineering |
Publisher | : |
Total Pages | : 60 |
Release | : 1990 |
Genre | : |
ISBN | : |
Download The Inviscid Stability of Supersonic Flow Past Heated Or Cooled Axisymmetric Bodies Book in PDF, Epub and Kindle
Author | : Institute for Computer Applications in Science and Engineering |
Publisher | : |
Total Pages | : 68 |
Release | : 1990 |
Genre | : |
ISBN | : |
Download The Inviscid Stability of Supersonic Flow Past a Sharp Cone Book in PDF, Epub and Kindle
Author | : Institute for Computer Applications in Science and Engineering |
Publisher | : |
Total Pages | : 78 |
Release | : 1989 |
Genre | : |
ISBN | : |
Download The Inviscid Axisymmetric Stability of the Supersonic Flow Along a Circular Cylinder Book in PDF, Epub and Kindle
Author | : National Aeronautics and Space Administration (NASA) |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 74 |
Release | : 2018-07-16 |
Genre | : |
ISBN | : 9781722814694 |
Download The Inviscid Axisymmetric Stability of the Supersonic Flow Along a Circular Cylinder Book in PDF, Epub and Kindle
The supersonic flow past a thin straight circular cylinder is investigated. The associated boundary layer flow (i.e., the velocity and temperature field) is computed; the asymptotic, far downstream solution is obtained, and compared with the full numerical results. The inviscid, linear, axisymmetric (temporal) stability of this boundary layer is also studied. A so called doubly generalized inflexion condition is derived, which is a condition for the existence of so called subsonic neutral modes. The eigenvalue problem (for the complex wavespeed) is computed for two freestream Mach numbers (2.8 and 3.8), and this reveals that curvature has a profound effect on the stability of the flow. The first unstable inviscid mode is seen to rapidly disappear as curvature is introduced, while the second (and generally the most important) mode suffers a substantially reduced amplification rate. Duck, Peter W. Unspecified Center...
Author | : Stephen James Shaw |
Publisher | : |
Total Pages | : 332 |
Release | : 1992 |
Genre | : |
ISBN | : |
Download Stability of the Boundary Layer Formed by Supersonic Flow Past Axisymmetric Bodies Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1572 |
Release | : 1992 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports 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 | : Wallace Dean Hayes |
Publisher | : Courier Corporation |
Total Pages | : 628 |
Release | : 2004-01-01 |
Genre | : Science |
ISBN | : 9780486432816 |
Download Hypersonic Inviscid Flow Book in PDF, Epub and Kindle
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.
Author | : |
Publisher | : |
Total Pages | : 538 |
Release | : 1991 |
Genre | : Aeronautics |
ISBN | : |
Download Aeronautical Engineering Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1126 |
Release | : 1991 |
Genre | : Government reports announcements & index |
ISBN | : |
Download Government Reports Annual Index Book in PDF, Epub and Kindle