Investigation made in Langley 7- by 10-foot tunnel; results indicate peak pressures on plug type spoiler slot aileron that may result in compressibility shock on plug aileron at high speed; max loads on plug aileron occurred in high speed condition for maximum up aileron deflection.
Pressure distribution over plug-type spoiler-slot aileron on tapered wing with full-span slotted flaps
Nat Advisory Committee Aeronautics -- Tech Note
1946
10 pages
Supp sheets, Bibliography
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English
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