Static stability and control characteristics of flight test model determined from force tests and lag characteristics of ailerons determined from roll-free stand tests; flight tests of model made through range of lift coefficient from 0.6 through stall by using data obtained from force tests to establish flight test conditions.
Comparison of lateral controllability with flap and plug ailerons on sweptback-wing model
Nat Advisory Committee Aeronautics -- Tech Note
1950
19 pages
Diagrs, Charts, Tables
Report
Englisch
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