Three-dimensional Flow of Ideal Gas Past Smooth Bodies PDF Download
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Author: Konstantin Ivanovich Babenko
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 532
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Book Description
Author: Konstantin Ivanovich Babenko
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 532
Get Book Here
Book Description
Author: Konstantin Ivanovich Babenko
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 520
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 478
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 970
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Book Description
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: Ira R. Schwartz
Publisher:
ISBN:
Category : Sonic boom
Languages : en
Pages : 472
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Book Description
Prediction methods for sonic boom generation and propagation with overpressure minimization in supersonic transport design and operation.
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 912
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Book Description
Author: E. B. Klunker
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 92
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Book Description
A computational technique, called the method of lines, is developed for computing the flow field about conical configurations at incidence in a supersonic flow. The method, which makes use of the self-similarity property, is developed for the nonlinear flow equations. The method has proved to be an efficient and versatile procedure for constructing the numerical solutions to conical flow problems. It has been successful in computing the flow about circular and elliptic cones at conditions where small regions of supersonic cross flow develop and for the conical delta wings where the region of supersonic cross flow is extensive. The calculations made for circular and elliptic cones as well as for the compression side of various conical delta wings are in good agreement with experiment except in regions where viscous effects become important.
Author: John V. Rakich
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 68
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Book Description
Characteristics method for determining three dimensional supersonic flow around inclined body of revolution.
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 1054
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Book Description
Author: Wallace D. Hayes
Publisher: Courier Corporation
ISBN: 0486160483
Category : Science
Languages : en
Pages : 628
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Book Description
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.
