Report describes calculations of transonic airflows about wing in wind tunnel. Basic equations of flow used in study are Reynolds-averaged Navier-Stokes equations in strong conservation-law form. Equations of flow incorporated into finite-difference computer code called TNS (Transonic Navier-Stokes). Computational grid generated by solution of partial differential equations yielding smooth meshes conforming to surfaces of wing and wind tunnel.
Calculations Of Transonic Flow About A Wing
NASA Tech Briefs ; 12 , 4
01.04.1988
Sonstige
Keine Angabe
Englisch
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