Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects - program documentation and test case / Sedat Biringen and Oden J. McMillen ; prepared for Langley Research Center under contract NAS1-1595.
The source listing of a computer code for calculating the flow fields in a supersonic free stream is given. The application of this code to an inlet on an airbreathing missile is also presented.
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. : [Springfield, Va.] :
National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Service],
1981.
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| Series: | NASA contractor report ;
NASA CR-3414. |
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Internet
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