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Supersonic Flutter of a 60© Delta Wing Encountered During the Flight Test of a Rocket-propelled Model

William T. Lauten

出版	National Advisory Committee for Aeronautics, 1954
URL	http://books.google.com.hk/books?id=xnyXGNmNfwMC&hl=&source=gbs_api
EBook	FULL_PUBLIC_DOMAIN

註釋

An analysis of the flight time-history records of a record-propelled 60 degree delta-wing airplane configuration indicate that wing flutter started during the accelerating portion of the flight at a Mach number of approximately 1.7 and continued through the peak Mach number of the test (M = 2.08) and during deceleration at least until telemeter failure at M = 1.4 and probably to an even lower speed. CW Doppler velocimeter data indicated that the wings did not fail during the flight.