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Results of initial wind-tunnel flutter experiments at low speed with a towed airplane model having a 40 degree sweptback wing of aspect ratio 3.62 equipped with pylon-mounted stores
Author:
Martina, Albert P.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L54K17
Link:
https://digital.library.unt.edu/ark:/67531/metadc60993/
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