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Experimental flutter results for cantilever-wing models at Mach numbers up to 3.0

W J Tuovila, J. L. Mccarty

Abstract

Report presenting experimental flutter testing at Mach numbers up to 3.0 using cantilever-wing models with 0 to 60 degree sweepback and 60 degree delta-wing models. The main variables explored were the high Mach number and center-of-gravity location on flutter trends. The theoretical results for flutter analyses were noted to be lower than the experimental results.

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Available abstract

Key concepts: Flutter, Mach number, Cantilever, Wing, Center of gravity, Supersonic speed, Degree (music), Structural engineering