Numerical research program helps establish "proof-of-concept" for newly developed higher-order panel method applicable to both subsonic and supersonic flows about nearly-arbitrary aircraft configurations. It is intended to solve variety of boundary-value problems in steady-subsonic or supersonic inviscid flow.
Advanced-panel pilot code
NASA Tech Briefs ; 4 , 2
1979-12-01
Miscellaneous
No indication
English
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