Nonlinear, three-dimensional effects computed from full potentialflow equation. Nonconical Relaxation program, NCOREL, employs new computational technique for prediction of inviscid, nonlinear supersonic aerodynamics. Unlike conventional linear potential equations, NCOREL utilizes full potential flow equation to predict formation of supercritical crossflow regions, embedded shocks, and bow shocks. NCOREL written in FORTRAN IV for batch execution.
Nonconical Relaxation for Supersonic Potential Flow
NASA Tech Briefs ; 10 , 2
1986-06-01
Sonstige
Keine Angabe
Englisch
Flow Past Nonconical Wings with Separation
AIAA | 1978
|Errata-Flow Past Nonconical Wings with Separation
AIAA | 1979
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