Model was string mounted wing body combination, and pressure measurements over one wing panel and one inboard and 2 outboard ailerons were obtained for angles of attack from 0 to 20° at deflections up to plus or minus 15°; positive deflections of ailerons caused significant added loadings over those wing sections not spanned by controls.
Investigation of wing and aileron loads due to deflected inboard and outboard ailerons on 4-percent-thick 30° sweptback wing at transonic speeds
NASA -- Tech Report
1961
282 pages
Report
English
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