Transonic Aeroelastic Modeling of the NACA 0012 Benchmark Wing

This work considers aeroelastic modeling of the NACA 0012 benchmark wing, a configuration previously tested in the Transonic Dynamics Tunnel for flutter. Numerical modeling is conducted within the ...

[1]  Robert T. Biedron,et al.  Recent Enhancements To The FUN3D Flow Solver For Moving-Mesh Applications , 2009 .

[2]  Robert M. Bennett,et al.  Experimental unsteady pressures at flutter on the Supercritical Wing Benchmark Model , 1993 .

[3]  Maynard C. Sandford,et al.  Unsteady pressure and structural response measurements on an elastic supercritical wing , 1988 .

[4]  Robert M. Bennett,et al.  NACA 0012 benchmark model experimental flutter results with unsteady pressure distributions , 1992 .

[5]  Earl H. Dowell,et al.  Improved Flutter Boundary Prediction for an Isolated Two-Degree-of-Freedom Airfoil , 2009 .

[6]  Walter A. Silva,et al.  Evaluation of linear, inviscid, viscous, and reduced-order modelling aeroelastic solutions of the AGARD 445.6 wing using root locus analysis , 2014 .

[7]  Steve L. Karman,et al.  Stabilized Finite Elements in FUN3D , 2017 .

[8]  William L. Kleb,et al.  Sketch-to-Solution: An Exploration of Viscous CFD with Automatic Grids , 2019, AIAA Aviation 2019 Forum.

[9]  R. J. Zwaan,et al.  Verification of calculation method for unsteady airloads in the prediction of transonic flutter , 1984 .

[10]  Frédéric Alauzet,et al.  Verification of Anisotropic Mesh Adaptation for Turbulent Simulations over ONERA M6 Wing , 2020 .

[11]  O. Bendiksen Review of unsteady transonic aerodynamics: Theory and applications , 2011 .

[12]  Robert W. Moses,et al.  Transport Wing Flutter Model Transonic Limit Cycle Oscillation Test , 2009 .

[13]  Frédéric Alauzet,et al.  High-order sonic boom modeling based on adaptive methods , 2010, J. Comput. Phys..

[14]  L. V. Zyl,et al.  Divergence and the p-k Flutter Equation , 2001 .

[15]  Andrew Arena,et al.  CFD-based aeroservoelastic predictions with comparisons to benchmark experimental data , 1999 .