论文信息 - Three-Dimensional Fluid-Structure Interactions of a Membrane Wing for Micro Air Vehicle Applications - 字舞流文

Three-Dimensional Fluid-Structure Interactions of a Membrane Wing for Micro Air Vehicle Applications

Yongsheng Lian | Wei Shyy | W. Shyy | Y. Lian

[1] Miguel R. Visbal,et al. DEVELOPMENT OF A THREE-DIMENSIONAL VISCOUS AEROELASTIC SOLVER FOR NONLINEAR PANEL FLUTTER , 2000 .

[2] M J Crompton,et al. Investigation of the separation bubble formed behind the sharp leading edge of a flat plate at incidence , 2000 .

[3] Wei Shyy,et al. Computational model of flexible membrane wings in steady laminar flow , 1995 .

[4] Wei Shyy,et al. Computational Fluid Dynamics with Moving Boundaries , 1995 .

[5] H.-T. Liu,et al. Unsteady aerodynamics of a Wortmann wing at low Reynolds numbers , 1992 .

[6] P. Jackson,et al. NUMERICAL ANALYSIS OF THREE-DIMENSIONAL ELASTIC MEMBRANE WINGS , 1987 .

[7] A. Gosman,et al. Solution of the implicitly discretised reacting flow equations by operator-splitting , 1986 .

[8] P. Thomas,et al. Geometric Conservation Law and Its Application to Flow Computations on Moving Grids , 1979 .

[9] Jean Duchon,et al. Splines minimizing rotation-invariant semi-norms in Sobolev spaces , 1976, Constructive Theory of Functions of Several Variables.