Nonlinear aerodyanmic characteristics of missile bodies computed. Program NOZVTX calculates nonlinear aerodynamic characteristics and flow fields of missile bodies at various angles-of-attack and roll in supersonic flow. Output includes geometry, centroids, and surface pressure of source panels and positions, strengths, and velocity components of shed vortexes. NOZVTX written in FORTRAN IV for batch execution.
Predicting Vortex Shedding in Supersonic Flow
NASA Tech Briefs ; 10 , 2
1986-06-01
Miscellaneous
No indication
English
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