Some Approximation Concepts for Structural Synthesis
暂无分享,去创建一个
[1] W. J. Stroud,et al. Minimum-weight stiffened shells with slight meridional curvature designed to support axial compressive loads. , 1969 .
[2] W. Lansing,et al. Application of Fully Stressed Design Procedures to Wing and Empennage Structures , 1971 .
[3] V. Venkayya. Design of optimum structures , 1971 .
[4] Jaroslaw Sobieszczanski,et al. A Mixed Optimization Method for Automated Design of Fuselage Structures , 1972 .
[5] Gary L. Giles,et al. Automated procedures for sizing aerospace vehicle structures /SAVES/ , 1972 .
[6] Roman Baldur,et al. Structural Optimization by Inscribed Hyperspheres , 1972 .
[7] R. E. Fulton,et al. An integrated computer system for preliminary design of advanced aircraft. , 1972 .
[8] M. F. Rubinstein,et al. Automated Structural Synthesis Using a Reduced Number of Design Coordinates , 1973 .
[9] Olaf O. Storaasli,et al. On the Accuracy of the Taylor Approximation for Structure Resizing , 1974 .
[10] L. A. Schmit,et al. A new structural analysis/synthesis capability - ACCESS , 1975 .