Minimum Weight Design of a Simply Supported Transversely Stiffened Plate Loaded in Shear

Stein a n d Fralich consider only infinitely long plates in t h e i r solution.1 However, from a s t u d y of similar papers3,6 which

T h e use of standard plate thicknesses is one of these factors. When choosing a standard plate thickness, b o t h the thickness above and t h e thickness below t h e o

Hohenemser K., 1952, Inc., 152

Stein Manuel, 1851, Simply Supported Plate with Transverse Stiffeners, NACA T N

Bleich F., 1952, Buckling Strength of Metal Structures, 1

Wang T. K., Journal of Applied Mechanics, 14, 269, 10.1115/1.4009732

Timoshenko S., 1936, Theory of Elastic Stability, 1

Shanley F. R., 1952, Weight-Strength Analysis of Aircraft Structures, 1

Budiansky Bernard, 1948, NACA T N

Kuhn Paul, 1952, A Summary of Diagonal Tension, Part I-Methods of Analysis, NACA T N 2 6 6 1

Anon, 1951, ANC-5, Munitions Board Aircraft Committee, U.vS.

Stowell E. Z., 1948, NACA T N

Prager William, 1951, Chap. 1

Shanley F. R., 1954, February

Seide Paul, 1953, NACA T N

Shone, 1933, RAE Report BA, 1080

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Horvay G., Quarterly of Applied Mathematics

10.2514/8.11513

Flax A. H., Journal of the Aeronautical Sciences, 14

Morse P. M., 1953, Methods of Theoretical Physics

Draper C. S., 1953, Instrument Engineering

Morduchow M., A, 1950, NACA T N 1999