TRANSEP Calculates flow field about low-speed single-element airfoil at high-angle-of-attack and high-lift conditions with massive boundary-layer separation. TRANSEP includes effects of weak viscous interactions and can be used for subsonic/transonic airfoil design and analysis. The approach used in TRANSEP is based on direct-inverse method and its ability to use either displacement surface or pressure as airfoil boundary condition.
High-Lift Separated Flow About Airfoils
NASA Tech Briefs ; 6 , 3
1982-12-01
Miscellaneous
No indication
English
Computation of separated flow about airfoils
British Library Conference Proceedings | 1993
|Lift on Airfoils with Separated Boundary Layers
AIAA | 1972
|British Library Online Contents | 1996
|British Library Conference Proceedings | 1996
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