A brief summary of recent 40- by 80-foot wind-tunnel investigations of large-scale models equipped with various high-lift devices is presented. The basic high-lift concepts that were investigated were the externally blown flap, the augmentor wing, and the rotating-cylinder flap. The scope of this paper is limited to a discussion of the wind-tunnel results in terms of maximum lift, descent performance, and pitch trim requirements.
A summary of recent large-scale research on high-lift devices
Conference on V/STOL and STOL aircraft ; 1966 ; Mountain View, CA, US
Conference on V/STOL and STOL aircraft ; NASA-SP-116
1966-04-04
Aufsatz (Konferenz)
Keine Angabe
Englisch
Summary of NACA investigations of high-lift devices
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