Comparison of Analytical and Experimental Steadyand 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 Steadyand Unsteady-pressure Distributions at Mach Number 0.78 for a High-aspect-ratio Supercritical Wing Model with Oscillating Control Surfaces
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Total Pages : 62
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ISBN-10 : NASA:31769000558448
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A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system