Tests to determine rolling moment, yawing moment, hinge moment and effect of midchord wing slots on characteristics of wing and aileron and tab; effect of leakage around tab hinge.
Investigation of aileron and tab of spring-tab lateral-control system in Langley 19-foot pressure tunnel
Nat Advisory Committee Aeronautics -- Tech Note
1947
34 pages
Report
English
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Aerodynamic tests of full-scale TBF-1 Aileron installation in Langley 16-foot high-speed tunnel
Engineering Index Backfile | 1944
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