Power-off tests conducted to determine dynamic stability of model with 42° swept back wing of aspect ratio 5.9 and taper ratio 0.45; results showed that, although wing alone was statically unstable longitudinally at moderate and high lift coefficients, complete model was practically stable over lift range for some horizontal tail positions.
Flight tests of airplane model with 42° swept-back wing in Langley free-plight tunnel
Nat Advisory Committee Aeronautics -- Tech Note
1947
14 pages
14 Supp plates
Report
English
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Flight tests of airplane model with 62° swept-back wing in Langley free-flight tunnel
Engineering Index Backfile | 1947
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