Flight investigation was made with sweptback wing aircraft fighter and wind tunnel investigation on semispan wing model in Langley 300-mph 7- by 10-ft tunnel; results on rolling effectiveness and hinge-moment characteristics of paddle spoilers at various subsonic speeds.
Limited flight and wind-tunnel investigation of paddle spoilers as lateral controls
NASA -- Tech Note
1959
20 pages
Report
Englisch
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Wind Tunnel and Flight Development of Spoilers for General Aviation Aircraft
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