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
Author: Sedat Biringen
Publisher:
Total Pages: 34
Release: 1980
Genre: Aerodynamics
ISBN:


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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
Pages: 34
Calculation of Two-Dimensional Inlet Flow Fields in a Supersonic Free Stream by an Implicit Marching Code with Nonorthogonal Mesh Generation
Language: en
Pages: 28
Authors: National Aeronautics and Space Administration (NASA)
Categories:
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: 44
Authors: Sedat Biringen
Categories: Aerodynamics
Type: BOOK - Published: 1981 - Publisher:

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