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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  • 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 Book Detail

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  • Release Date : 1984
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  • Pages : 62
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  • File Size : 54,54 MB
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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 by PDF Summary

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Aeronautical Engineering

Aeronautical Engineering

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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