Comparison of Analytical and Experimental Subsonic Steady and Unsteady Pressure Distributions for a High-aspect-ratio-supercritical Wing Model with Oscillating Control Surfaces

Comparison of Analytical and Experimental Subsonic Steady and Unsteady Pressure Distributions for a High-aspect-ratio-supercritical Wing Model with Oscillating Control Surfaces
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Total Pages : 58
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ISBN-10 : NASA:31769000557614
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Rating : 4/5 (14 Downloads)

Book Synopsis Comparison of Analytical and Experimental Subsonic Steady and Unsteady Pressure Distributions for a High-aspect-ratio-supercritical Wing Model with Oscillating Control Surfaces by :

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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