Calculation Of Two Dimensional Inlet Flow Fields In A Supersonic Free Stream
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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
Author | : Sedat Biringen |
Publisher | : |
Total Pages | : 34 |
Release | : 1980 |
Genre | : Aerodynamics |
ISBN | : |
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Type: BOOK - Published: 2018-07-25 - Publisher: Createspace Independent Publishing Platform
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
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