Computer program analyzes performance of jet-flap wings. Fast and easy-to-use prediction technique, it generates accurate solutions for wide range of wing geometries and trailing-edge jet momentum distributions. Analysis is based on optimized vortex-lattice approach and results in rapid convergence of both overall and distributed loadings.
Aerodynamic performance of jet-flap wings
NASA Tech Briefs ; 4 , 4
1980-06-01
Miscellaneous
No indication
English
SAGE Publications | 2021
|Engineering Index Backfile | 1961
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