FLIGHT TESTS AND WIND-TUNNEL MEASUREMENTS ON AEROFOILS WITH BOUNDARY LAYER SUCTION FOR INCREASING MAXIMUM LIFT
International Council of the Aeronautical Sciences ; 1964 ; Paris , France
1964-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Wind tunnel tests of aerofoils with pilot planes
SLUB | 1929
|Wind tunnel tests on aerofoils at negative incidences
SLUB | 1930
|Wind tunnel tests on aerofoils at negative incidences
TIBKAT | 1931
|Wind tunnel tests of aerofoils R.A.F. 38 and 48
SLUB | 1933
|Flight tests on aircraft Model RW 3a having boundary layer suction to increase maximum lift
Engineering Index Backfile | 1963
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