Some Effects Of Taper Ratio On The Transonic Flutter Characteristics Of A Series Of Thin Cantilever Wings Having A Sweptback Angle Of 45 And An Aspect Ratio 4 0


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Index of NASA Technical Publications


Index of NASA Technical Publications

Author: United States. National Aeronautics and Space Administration

language: en

Publisher:

Release Date: 1960


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Index of NASA Technical Publications


Index of NASA Technical Publications

Author:

language: en

Publisher:

Release Date: 1959


DOWNLOAD