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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