Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis
暂无分享,去创建一个
[1] G. N. Vanderplaats,et al. ADS: A FORTRAN program for automated design synthesis: Version 1.10 , 1984 .
[2] Oktay Baysal,et al. Airfoil Shape Optimization Using Sensitivity Analysis on Viscous Flow Equations , 1993 .
[3] Michael J. Mann,et al. Aerodynamic design of supersonic cruise wings with a calibrated linearized theory , 1994 .
[4] Oktay Baysal,et al. Aerodynamic shape optimization using preconditioned conjugate gradient methods , 1994 .
[5] O. Baysal,et al. Aerodynamic shape optimization via sensitivity analysis on decomposed computational domains , 1992 .
[6] X S Bauer Steven,et al. The Natural Flow Wing-Design Concept , 1992 .
[7] Oktay Baysal,et al. Aerodynamic design optimization using sensitivity analysis and computational fluid dynamics , 1991 .
[8] Oktay Baysal,et al. Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle , 1992 .
[9] O. Baysal,et al. Aerodynamic Sensitivity Analysis Methods for the Compressible Euler Equations , 1991 .
[10] Oktay Baysal,et al. Design optimization using variational methods and CFD , 1994 .
[11] O. Baysal,et al. Design of 3-D Nacelle near Flat-Plate Wing Using Multiblock Sensitivity Analysis (ADOS) , 1994 .
[12] W. K. Anderson,et al. Navier-Stokes Computations of Vortical Flows Over Low-Aspect-Ratio Wings , 1987 .
[13] G. Burgreen,et al. Aerodynamic Shape Optimization Using Sensitivity Analysis on Third-Order Euler Equations , 1993 .