High fidelity computational simulation of a membrane wing airfoil von Gordnier, R.E.

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Aeroelastic prediction of the limit cycle oscillations of a cropped delta wing von Attar, P.J., Gordnier, R.E.

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DEVELOPMENT OF A THREE-DIMENSIONAL VISCOUS AEROELASTIC SOLVER FOR NONLINEAR PANEL FLUTTER von GORDNIER, R.E., VISBAL, M.R.

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Numerical simulation of the interaction of a transitional boundary layer with a 2-D flexible panel in the subsonic regime von Visbal, M.R., Gordnier, R.E.

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Computation of the aeroelastic response of a flexible delta wing at high angles of attack von Gordnier, R.E., Visbal, M.R.

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High-Fidelity Computations of Moving and Flexible Wing Sections with Application to Micro Air Vehicles von Gordnier, R.E., Visbal, M.R., Galbraith, M.C.

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High-Fidelity Simulations for Maneuvering Unmanned Combat Air Vehicle Configurations von Gordnier, R.E., Visbal, M.R., Sherer, S.E.

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Transonic flow solutions using a composite velocity procedure for potential, Euler and RNS equations von Gordnier, R.E., Rubin, S.G.

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Higher-Order Accurate Computations of Maneuvering Unmanned Combat Air Vehicle Configurations von Gordnier, R.E., Visbal, M.R., Sherer, S.E.

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CFD-Based HPCMP Systems Assessment Using AERO, AVUS, and OVERFLOW-2 von Cable, S.B., Oppe, T.C., Ward, W.A., Gordnier, R.E., Burnley, V.S., Grismer, M.J., Campbell, R.L., Burning, P.G.

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