Optimum design of stiffened shear webs with supplementary skin stabilisation

International Journal of Solids and Structures - Tập 12 - Trang 791-802 - 1976
D.M. Richards1
1Aircraft Design Division, College of Aeronautics, Cranfield Institute of Technology, Cranfield, Bedford MK430AL, England

Tài liệu tham khảo

Kuhn, 1952, A Summary of Diagonal Tension. Part I, Analysis., NACA TN2661

Kuhn, 1952, A Summary of Diagonal Tension. Part 2, Tests., NACA TN2662

Symonds, 1956, Minimum weight design of a simply supported transversely stiffened plate loaded in shear, J. Aero. Sci., 23, 9685, 10.2514/8.3634

Shanley, 1952, Weight-Strength Analysis of Aircraft Structures, 38

Rothwell, 1968, The buckling of shallow corrugated webs in shear, J.R. Aero. S., 72

Parsons, 1973, The optimum distribution of diagonal stiffeners reinforcing a clamped infinitely long plate buckling in shear, Aeronautical J.R.Ae.S., 77

Laakso, 1974, Evaluation of a Metal Shear Web Selectively Reinforced with Filamentary Composites for Space Shuttle Application., NASA CR-2409

Stein, 1949, Critical Shear Stress of Infinitely Long, Simply Supported Plate with Transverse Stiffeners, NACA TN 1851

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1964, Engineering Sciences Data Sheets 02.03.02

Timoshenko, 1961, Theory of Elastic Stability, 405

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Thông tin xuất bản

International Journal of Solids and Structures

Tập 12

791-802

Thông tin tác giả