Physical concepts of boundary layer control for high lift; successful flight application of two of these concepts to Air Force aircraft; F-86 leading edge suction project at NACA Ames Aeronautical Laboratory; tests on F-86 wing in Ames full scale wind tunnel; XC-123 D program tests in full scale wind tunnel at Langley Field. (see also Soc Automotive Engrs -- J v 63 n 7 July 1955 p 44-6)
Some experiments in application of boundary layer control
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1955 Boundary layer
1955
6 pages
Aufsatz (Konferenz)
Englisch
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Some experiments in application of boundary-layer control
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