Low-speed wind-tunnel tests on a wing-fuselage model with area suction through perforations at the leading-edge flap knee
1970
55 S.
Ill., graph. Darst.
Buch
Englisch
DDC: | 629.13/008 s |
Wind-tunnel tests on model wing with fowler flap and specially developed leading-edge clot
Engineering Index Backfile | 1933
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