Wind tunnel tests of the stalling properties of an 8 per cent thick symmetrical section with nose suction through a porous surface
1953
14 S.
graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
DDC: | 629.13432 |
Wind-tunnel tests on a 30 per cent. suction wing
TIBKAT | 1945
|Wind-tunnel tests on the NPL 434 nose-slot suction aerofoil
TIBKAT | 1955
|