It is shown from elementary considerations that in zero incidence case lift coefficient and pressure distribution can be obtained directly (i.e. without solving flow problem fully) when jet momentum coefficient is small; formula is given.
Some simple results for two-dimensional jet-flap aerofoils
Aeronautical Quarterly
Aeronautical Quarterly ; 9 , Part 4
1958
12 pages
Aufsatz (Zeitschrift)
Englisch
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