Numerical Solution Of Supersonic Viscous Flow Over Blunt Delta Wings
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Author | : |
Publisher | : |
Total Pages | : 36 |
Release | : 1980 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Numerical Solution of Supersonic Viscous Flow Over Blunt Delta Wings Book in PDF, Epub and Kindle
Author | : Franklyn B. Fuller |
Publisher | : |
Total Pages | : 52 |
Release | : 1961 |
Genre | : Aerodynamics |
ISBN | : |
Download Numerical Solutions for Supersonic Flow of an Ideal Gas Around Blunt Two-dimensional Bodies Book in PDF, Epub and Kindle
Author | : Susan Naomi McMillin |
Publisher | : |
Total Pages | : 108 |
Release | : 1990 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Navier-Stokes and Euler Solutions for Lee-side Flows Over Supersonic Delta Wings Book in PDF, Epub and Kindle
Author | : Bernard Mazelsky |
Publisher | : |
Total Pages | : 82 |
Release | : 1967 |
Genre | : |
ISBN | : |
Download Research on Hypersonic Flow of Blunt Delta Wings. Part I. Theoretical and Experimental Study of a 70-degree Blunt Delta Wing for Low Angles of Attack at Supersonic and Hypersonic Speeds Book in PDF, Epub and Kindle
The object of the present analysis is to investigate the high-speed aerodynamic properties of a blunt delta wing at low angles of attack where the maximum lift to drag ratio occurs. Oguchi's solution of hypersonic flow over a blunt leading edge flat plate at zero incidence is extended to three dimensional delta wings at angle of attack. The shock wave shapes and pressure distributions were obtained by employing the oblique shock relations at the windward sides of the Prandtl-Meyer equations at the leeward side of the wing. The total lift and drag of the wing due to pressure and skin friction were computed by numerical integration using the IBM 7094 computer. The present calculated aerodynamic forces generally agree with the experimental data at the high supersonic Mach numbers (M approx.> or = 4) and lower thickness ratio of the wing which is a 70-degree swept slab sided delta wing with a cylindrical leading edge. (Author).
Author | : V.Z. Parton |
Publisher | : Routledge |
Total Pages | : 352 |
Release | : 2018-03-29 |
Genre | : Technology & Engineering |
ISBN | : 1351412949 |
Download Super- and Hypersonic Aerodynamics and Heat Transfer Book in PDF, Epub and Kindle
Recent government and commercial efforts to develop orbital and suborbital passenger and transport aircraft have resulted in a burgeoning of new research. The articles in this book, translated from Russian, were contributed by the world's leading authorities on supersonic and hypersonic flows and heat transfer. This superb book addresses the physics and engineering aspects of ultra high-speed aerodynamic problems. Thorough coverage is given to an array of specific problem-solving equations. Super- and Hypersonic Aerodynamics and Heat Transfer will be essential reading for all aeronautical engineers, mechanical engineers, mathematicians, and physicists involved in this exciting field of research.
Author | : Peter A. Gnoffo |
Publisher | : |
Total Pages | : 100 |
Release | : 1978 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Forebody and Afterbody Solutions of the Navier-Stokes Equations for Supersonic Flow Over Blunt Bodies in a Generalized Orthogonal Coordinate System 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 | : |
Publisher | : |
Total Pages | : 1878 |
Release | : 1961 |
Genre | : Government publications |
ISBN | : |
Download Monthly Catalog of United States Government Publications Book in PDF, Epub and Kindle
Author | : Albert George Bennett |
Publisher | : |
Total Pages | : 56 |
Release | : 1964 |
Genre | : |
ISBN | : |
Download A Numerical Solution for the Downwash Onto a Delta Wing Due to a Vortex Pair in Supersonic Flow Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 646 |
Release | : 1983 |
Genre | : Aeronautics |
ISBN | : |
Download AIAA 83-0204 - AIAA 83-0309 Book in PDF, Epub and Kindle