论文信息 - Sequential use of conceptual MDO and panel sizing methods for aircraft wing design - 字舞流文

Sequential use of conceptual MDO and panel sizing methods for aircraft wing design

J. R. Banerjee | M. Lillico | M. H. Patel | G. T. S. Done | Richard Butler | R. Butler | J. Banerjee | G. Done | M. Patel | M. Lillico

[1] D. J. Neill,et al. ASTROS - A multidisciplinary automated structural design tool , 1987 .

[2] P. Bartholomew,et al. Computer-Aided Optimization of Aircraft Structures , 1990 .

[3] T. A. Weisshaar,et al. Aeroelastic tailoring - Theory, practice, and promise , 1984 .

[4] Stephen M. Batill,et al. FASTOP: A Flutter and Strength optimization Program for Lifting-Surface Structures , 1977 .

[5] Richard Butler,et al. Optimum design of composite stiffened wing panels — a parametric study , 1995, The Aeronautical Journal (1968).

[6] Fred W. Williams,et al. Optimum design using VICONOPT, a buckling and strength constraint program for prismatic assemblies of anisotropic plates , 1992 .