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Experimental Transonic Flutter Characteristics of an Untapered, 45 Degree Sweptback, Aspect-ratio-4 Wing

C. L. Ruhlin

Abstract

Report presenting the flutter characteristics of an untapered, 45 degree sweptback, aspect-ratio-4 wing at a range of Mach numbers. The results from NACA RM L55E19a are included along with additional information regarding the models, the tests, and the results of the flutter calculations.

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Available abstract

Key concepts: Flutter, Transonic, Wing, Aspect ratio (aeronautics), Degree (music), Airfoil, Mach number, Aerodynamics