High-lift wing concepts being considered for application to commercial STOL transports are discussed. The flow patterns which produce dynamic loads on these wings are indicated. Measurements of surface pressure and acceleration on a one-half-scale model of an externally blown double-slotted flap are reported. Root-mean-square values, power spectra, and scaling parameters are shown.
Dynamic loading of aircraft surfaces due to jet exhaust impingement
01.05.1973
Aufsatz (Konferenz)
Keine Angabe
Englisch
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