Comparison of analytical and experimental steady- and unsteady-pressure distributions at Mach number 0.78 for a high-aspect-ratio supercritical wing model with oscillating control surfaces

Comparison of analytical and experimental steady- and unsteady-pressure distributions at Mach number 0.78 for a high-aspect-ratio supercritical wing model with oscillating control surfaces

by William E McCain

Book 84589 of NASA technical memorandum --

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