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Evaluation of four subcritical response methods for on-line prediction flutter onset in wind-tunnel tests. [conducted in the Langley Transonic Dynamics Tunnel

C. L. Ruhlin, Judith J. Watson, R. H. Ricketts, R. V. Doggett

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Key concepts: Transonic, Flutter, Wind tunnel, Subsonic and transonic wind tunnel, Line (geometry), Aerodynamics, Engineering, Aeronautics

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Evaluation of four subcritical response methods for on-line prediction flutter onset in wind-tunnel tests. [conducted in the Langley Transonic Dynamics Tunnel — Research Paper | ScholarLens