Investigation to determine severity of dynamic stability and control problems; force and tuft tests made to determine static stability and wing stall characteristics, and calculations made to determine boundary of zero damping of lateral oscillation.
Flight tests of airplane model with 62° swept-back wing in Langley free-flight tunnel
Nat Advisory Committee Aeronautics -- Tech Note
1947
14 pages
10 Supp plates, Bibliography
Report
English
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Flight tests of airplane model with 42° swept-back wing in Langley free-plight tunnel
Engineering Index Backfile | 1947
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