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Flutter Investigation in the High Subsonic and Transonic Speed Range on Cantilever Delta-wing Plan Forms with Leading-edge Sweepback of 60 Degrees, 53 Degrees 8', and 45 Degrees

William T Lauten, Marvin F Burgess

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Abstract

Report presenting results of flutter testing on three cantilever delta-wing plan forms at a range of Mach numbers. The time and location of flutter and results of the flutter calculations are provided for each of the wings.

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What this paper is about

Report presenting results of flutter testing on three cantilever delta-wing plan forms at a range of Mach numbers. The time and location of flutter and results of the flutter calculations are provided for each of the wings.

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Available abstract

Report presenting results of flutter testing on three cantilever delta-wing plan forms at a range of Mach numbers. The time and location of flutter and results of the flutter calculations are provided for each of the wings.

Key concepts: Flutter, Transonic, Cantilever, Delta wing, Wing, Leading edge, Mach number, Structural engineering

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Flutter Investigation in the High Subsonic and Transonic Speed Range on Cantilever Delta-wing Plan Forms with Leading-edge Sweepback of 60 Degrees, 53 Degrees 8', and 45 Degrees — Research Paper | ScholarLens