Calculation Of Two Dimensional Inlet Flow Fields In A Supersonic Free Stream
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Language: en
Pages: 28
Pages: 28
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
Language: en
Pages: 172
Pages: 172
Type: BOOK - Published: 1980 - Publisher:
Language: en
Pages: 34
Pages: 34
Type: BOOK - Published: 1980 - Publisher:
Language: en
Pages: 32
Pages: 32
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Language: en
Pages: 178
Pages: 178
Type: BOOK - Published: 1980 - Publisher: