Report describes numerical simulations of transonic flow of air about isolated wing and about wing and fuselage (not tail assembly) of F-16A aircraft. Fast, diagonalized Beam-Warming numerical-integration algorithm for solution of Euler and Navier-Stokes equations applied via Transonic Navier-Stokes computer program, using computational grids divided into zones of coarse and finer meshes.
Navier-Stokes Computations On Zonal Grids
NASA Tech Briefs ; 15 , 12
1991-12-01
Miscellaneous
No indication
English
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