VORSTAB program developed to calculate lateral-directional characteristics of nonplanar wing/body combinations in subsonic flow. Mathematically determines effects of edge-separated vortex flow, including augmented vortex lift, strake-induced downwash, and vortex breakdown. VORSTAB written in FORTRAN IV.
Calculating Aerodynamic-Stability Derivatives
NASA Tech Briefs ; 10 , 4
1986-07-01
Miscellaneous
No indication
English
Methodology for calculating aerodynamic sensitivity derivatives
Tema Archive | 1992
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