Paper reviews history of subject, examines definitions of thrust recovery, especially in light of recent experimental work done at Stanford University; data obtained from tests of jet augmented flap model in National Aeronautical Establishment low speed wind tunnel are presented; analysis of data revealed drag due to lift to be not only expected function of jet thrust coefficient, but also function of jet or flap angle; possible reasons for behavior and implication of thrust recovery for STOL aircraft are considered.
Jet-flap thrust recovery -- Its history and experimental realization
Can Aeronautics Space J
Canadian Aeronautics and Space Journal ; 11 , n 5
1965
9 pages
Aufsatz (Zeitschrift)
Englisch
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