Three-dimensional Inviscid Flow about Supersonic Blunt Cones at Angle of Attack PDF Download
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Author: M. J. Abbett
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 126
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Book Description
The solution for the steady three-dimensional inviscid flow about supersonic blunt cones at angle of attack is obtained by coupling a direct time-dependent solution for the subsonic portion of the shock layer with steady state numerical afterbody solution. An outline is given covering the coupling scheme and the use of the resulting Fortran computer code.
Author: M. J. Abbett
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 126
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Book Description
The solution for the steady three-dimensional inviscid flow about supersonic blunt cones at angle of attack is obtained by coupling a direct time-dependent solution for the subsonic portion of the shock layer with steady state numerical afterbody solution. An outline is given covering the coupling scheme and the use of the resulting Fortran computer code.
Author: G. Moretti
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
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Book Description
Comparisons are made between the cylindrical and polar coordinate system used in determining the three-dimensional shock layer flow over the nose region of a blunted supersonic vehicle. Jusfification for the development of a polar coordinate system is given and an outline for such development is presented. Results from the polar coordinate system are given as is the limiting useful range.
Author: G. Moretti
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 88
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Book Description
Author: General Applied Science Laboratories (Westbury, Nassau County, N.Y.)
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 130
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Book Description
Author: G. Moretti
Publisher:
ISBN:
Category :
Languages : en
Pages : 80
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Book Description
Author: Dale Anderson
Publisher: Taylor & Francis
ISBN: 1466578300
Category : Science
Languages : en
Pages : 763
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Book Description
Thoroughly updated to include the latest developments in the field, this classic text on finite-difference and finite-volume computational methods maintains the fundamental concepts covered in the first edition. As an introductory text for advanced undergraduates and first-year graduate students, Computational Fluid Mechanics and Heat Transfer, Thi
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1572
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 452
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Book Description
Author: V.Z. Parton
Publisher: Routledge
ISBN: 1351412949
Category : Technology & Engineering
Languages : en
Pages : 352
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Book Description
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:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
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Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
