论文信息 - The “CST” Universal Parametric Geometry Representation Method, Recent Extensions and Applications - 字舞流文

The “CST” Universal Parametric Geometry Representation Method, Recent Extensions and Applications

Brenda M. Kulfan | B. Kulfan

[1] Richard H. Burkhart,et al. TRANAIR - A computer code for transonic analyses of arbitrary configurations , 1987 .

[2] John E. Bussoletti,et al. "Fundamental" Parameteric Geometry Representations for Aircraft Component Shapes , 2006 .

[3] Wu Li,et al. Options for Robust Airfoil Optimization under Uncertainty , 2002 .

[4] H. Sobieczky. Parametric Airfoils and Wings , 1999 .

[5] Helmut Sobieczky,et al. AERODYNAMIC DESIGN AND OPTIMIZATION TOOLS ACCELERATED BY PARAMETRIC GEOMETRY PREPROCESSING , 2000 .

[6] A New Supersonic Wing Far-Field Composite Element Wave Drag Optimization Method , “ FCE ” , 2008 .

[7] Raymond M. Hicks,et al. Wing design by numerical optimization , 1977 .

[8] J. Samareh. Survey of Shape Parameterization Techniques for High-Fidelity Multidisciplinary Shape Optimization , 2001 .

[9] B. Kulfan. Universal Parametric Geometry Representation Method , 2008 .

[10] Andy J. Keane,et al. Concise Orthogonal Representation of Supercritical Airfoils , 2001 .

[11] Deepak Om,et al. TRANAIR Packaging for Ease-of-Use in Wing Design , 1998 .

[12] M. E. Manro,et al. Aeroelastic loads prediction for an arrow wing. Task 2: Evaluation of semi-empirical methods , 1983 .