A boundary-layer integral approach is combined with a finite-difference relaxation method to calculate viscous interactions between separated flows at subsonic and transonic velocities. Results are obtained for separated laminar flows on circular-arc airfoils at zero angle of attack and are compared with data of Collins (1972). Inviscid and viscous flows are covered.
Calculation of separated flows at subsonic and transonic speeds
International Conference on Numerical Methods in Fluid Mechanics ; 1972 ; Paris, France
1973-01-01
Miscellaneous
No indication
English
A Study of Isolated Nacelle Flows at Subsonic and Transonic Speeds
British Library Conference Proceedings | 1998
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