AIRFOILS-NACA 66,2-216-CHAR , MOMENTS & ORDINATES LOW-DRAG; CONTROL STICKS-FORCES; MACH NUMBER; PRESSURE DISTRIBUTION-AIRFOILS-NACA 66,2-216; AILERONS, BALANCED - SEALED-GAP; AILERONS, BALANCED - HINGE MOMENTS; AILERONS - WIND TUNNEL TESTS; FLYING, HIGH-SPEED; WIND TUNNEL TESTS-NACA-STABILITY;
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