Results and discussion of lateral control investigation; data obtained through large angle-of-attack range and at Mach numbers from 0.13 to 0.71.
High-speed wind-tunnel investigation of NACA 65-210 semispan wing equipped with plug and retractable ailerons and full-span slotted flap
Nat Advisory Committee Aeronautics -- Tech Note
1948
81 pages
Bibliography
Report
Englisch
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Engineering Index Backfile | 1949
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