Study by Fairchild Aircraft Division of possibility of applying boundary layer control to C-119 airplane in order to reduce minimum flying speed and takeoff and landing distances; three systems studied, all of which showed merit; extensive aerodynamic data correlating boundary layer thickness with flap condition, lift coefficient, and power, derived.
Boundary layers measured in flight tests
Aero Digest
Aero Digest ; 72 , n 5
1956
11 pages
Aufsatz (Zeitschrift)
Englisch
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BOUNDARY-LAYER STABILITY ANALYSIS OF FLIGHT-MEASURED TRANSITION DATA
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