A Supersonic, Three-dimensional Code for Flow Over Blunt Bodies PDF Download
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Author: D. S. Chaussee
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32
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Book Description
Author: D. S. Chaussee
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32
Get Book Here
Book Description
Author: D. S. Chaussee
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 212
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Book Description
Author: D. S. Chaussee
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32
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Book Description
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724222978
Category :
Languages : en
Pages : 28
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Book Description
A computer code is described which may be used to calculate the steady, supersonic, three-dimensional, inviscid flow over blunt bodies. The theoretical and numerical formulation of the problem is given (shock-capturing, downstream marching), including exposition of the boundary and initial conditions. The overall flow logic of the program, its usage, accuracy, and limitations are discussed. Chaussee, D. S. and Mcmillan, O. J. Unspecified Center NASA-CR-3223, NEAR-TR-189 NAS1-15305
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 252
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 252
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1572
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1094
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1094
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 656
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