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DETERMINATION OF AIRCRAFT STRUCTURE WHIRL FLUTTER STABILITY BOUNDARIES BY MEANS OF OPTIMIZATION BASED SOLUTION
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Čečrdle, J.
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Cecrdle_FT
version 1
Cecrdle_FT.pdf
[1.46 MB]
13 Nov 2014, 09:18
Original version of the author's contribution as presented on CD, , page 112.
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