Pitch rate/sideslip effects on leading-edge extension...

Journal of Aircraft 1992 / 07 Vol. 29; Iss. 4

Pitch rate/sideslip effects on leading-edge extension vortices of anF/A-18 aircraft model

HEBBAR, SHESHAGIRI K., PLATZER, MAX F., CAVAZOS, ODILON V.
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Volume:
29
Language:
english
Journal:
Journal of Aircraft
DOI:
10.2514/3.46230
Date:
July, 1992
File:
PDF, 530 KB
english, 1992
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