Calculation Of Two Dimensional Inlet Flow Fields In A Supersonic Free Stream By An Implicit Marching Code With Nonorthogonal Mesh Generation

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Calculation of two-dimensional inlet flow fields in a supersonic free stream by an implicit marching code with nonorthogonal mesh generation

Calculation of two-dimensional inlet flow fields in a supersonic free stream by an implicit marching code with nonorthogonal mesh generation
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Total Pages : 34
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ISBN-10 : STANFORD:36105024668126
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Book Synopsis Calculation of two-dimensional inlet flow fields in a supersonic free stream by an implicit marching code with nonorthogonal mesh generation by : Sedat Biringen

Download or read book Calculation of two-dimensional inlet flow fields in a supersonic free stream by an implicit marching code with nonorthogonal mesh generation written by Sedat Biringen and published by . This book was released on 1980 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:


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Calculation of two-dimensional inlet flow fields in a supersonic free stream by an implicit marching code with nonorthogonal mesh generation
Language: en
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Calculation of Two-Dimensional Inlet Flow Fields in a Supersonic Free Stream by an Implicit Marching Code with Nonorthogonal Mesh Generation
Language: en
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Authors: National Aeronautics and Space Administration (NASA)
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Type: BOOK - Published: 2018-07-25 - Publisher: Createspace Independent Publishing Platform

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An implicit, shock-capturing finite-difference code which is used to calculate two-dimensional inlet flow fields in a supersonic free stream is explained. The E
Calculation of Two-dimensional Inlet Flow Fields in a Supersonic Free Stream
Language: en
Pages: 172
Authors: Sedat Biringen
Categories: Aerodynamics
Type: BOOK - Published: 1980 - Publisher:

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Calculation of Two-dimensional Inlet Flow Fields by an Implicit Method Including Viscous Effects
Language: en
Pages: 32
Authors: Sedat Biringen
Categories: Aerodynamics
Type: BOOK - Published: 1981 - Publisher:

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Inlet flow fields for airbreathing missiles are calculated by the adaptation of a two dimensional computational method developed for the flow around airfoils. A