Computational Study of Stall Flutter of the Benchmark Supercritical Wing
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[1] D. Raveh,et al. Stall Flutter of the Benchmark Supercritical Wing at High Angles of Attack , 2023, AIAA SCITECH 2023 Forum.
[2] Gecheng Zha,et al. Stall flutter simulation of a transonic axial compressor stage using a fully coupled fluid-structure interaction , 2017 .
[3] Jennifer Heeg,et al. Investigating the Transonic Flutter Boundary of the Benchmark Supercritical Wing , 2017 .
[4] Jennifer Heeg,et al. Experimental Data from the Benchmark SuperCritical Wing Wind Tunnel Test on an Oscillating Turntable , 2013 .
[5] Oddvar O. Bendiksen,et al. High-Altitude Limit Cycle Flutter of Transonic Wings , 2007 .
[6] Oddvar O. Bendiksen,et al. Transonic Limit Cycle Flutter of High-Aspect-Ratio Swept Wings , 2006 .
[7] Koji Isogai,et al. Shock-Stall Flutter of a Two-Dimensional Airfoil , 2004 .
[8] Jeffrey P. Thomas,et al. Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter, and Limit-Cycle Oscillations , 2001 .
[9] Philippe R. Spalart,et al. Trends in turbulence treatments , 2000 .
[10] Michael A. Leschziner,et al. Average-State Jacobians and Implicit Methods for Compressible Viscous and Turbulent Flows , 1997 .
[11] J. Edwards,et al. Comparison of eddy viscosity-transport turbulence models for three-dimensional, shock-separated flowfields , 1994 .
[12] David J. Piatak,et al. A New Forced Oscillation Capability for the Transonic Dynamics Tunnel , 2002 .
[13] Robert M. Bennett,et al. Experimental unsteady pressures at flutter on the Supercritical Wing Benchmark Model , 1993 .
[14] Robert M. Bennett,et al. NACA 0012 benchmark model experimental flutter results with unsteady pressure distributions , 1992 .