lift of supersonic airfoil at subsonic regime
lift of supersonic airfoil at subsonic regime
(OP)
I would like to know how the lift is created for a supersonic airplane before there is a shock wave created at the leading edge of the wings, For example during take-off and landing. I am curious to know that and have done no course in transonic and supersonic aerodyanmics!
Thank you.
Thank you.





RE: lift of supersonic airfoil at subsonic regime
RE: lift of supersonic airfoil at subsonic regime
RE: lift of supersonic airfoil at subsonic regime
to my know the lift crated during take-off and landing on civilian supersonic airplane is similar to what butelja said, vortex lift at high angles of attack. This is the reason, why concorde has such a adjustable cockpit.
cheers