Highly Compact Supersonic Inlet Design Optimization
暂无分享,去创建一个
[1] C. C. Law,et al. ParaView: An End-User Tool for Large-Data Visualization , 2005, The Visualization Handbook.
[2] Peter A. Cavallo,et al. Hybrid, viscous, unstructured mesh solver for propulsive applications , 1998 .
[3] M. Powell. A Direct Search Optimization Method That Models the Objective and Constraint Functions by Linear Interpolation , 1994 .
[4] Mohamed S. Ebeida,et al. Dakota, a multilevel parallel object-oriented framework for design optimization, parameter estimation, uncertainty quantification, and sensitivity analysis version 6.0 theory manual , 2020 .
[5] Doyle Knight,et al. Three dimensional optimization of supersonic inlets , 1999 .
[6] C. M. Reeves,et al. Function minimization by conjugate gradients , 1964, Comput. J..
[7] David L. Rodriguez. Multidisciplinary Optimization of a Supersonic Inlet Using a Cartesian CFD Method , 2004 .
[8] Andrew Gelsey,et al. High-Performance Supersonic Missile Inlet Design Using Automated Optimization , 1997 .
[9] Ashvin Hosangadi,et al. Upwind unstructured scheme for three-dimensional combusting flows , 1996 .
[10] Michael S. Eldred,et al. DAKOTA : a multilevel parallel object-oriented framework for design optimization, parameter estimation, uncertainty quantification, and sensitivity analysis. Version 5.0, user's reference manual. , 2010 .