Results indicate that loading over ailerons was established by wing flow characteristics, and loading shapes were irregular in transonic speed range; other findings.
Normal-force and hinge-moment characteristics at transonic speeds of flap-type ailerons at three spanwise locations on 4-percent-thick sweptback-wing-body model and pressure-distribution measurements on inboard aileron
NASA -- Tech Note
1961
55 pages
Report
English
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Engineering Index Backfile | 1961
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