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Selected Publications:
Leggett, D.M.A., “On the elastic stability of a rectangular plate when subjected to variable edge thrust”, Proceedings of the Cambridge Phil. Soc., Vol. 31, 1935, p. 368
Leggett, D. M. A. The elastic stability of a long and slightly bent plate under uniform shear. Proc. R. Soc., 1937, A162, 62–83.
Leggett, D.M.A., “The buckling of a square panel under shear when one pair of opposite edges is clamped”, R. & M. No. 1991, 1941
Williams, D., Leggett, D. M. A., and Hopkins, H. G. 1941. Flat Sandwich Panels Under Compressive End Loads. British Royal Aircraft Establishment Report No. A. D. 3 174
Leggett, D.M.A. and Hopkins, H.G., “Sandwich panels and cylinders under compressive end loads”, R. & M. No. 2262, British A.R.C., 1942
Leggett, D. M. A., and Jones, R. P. N., "The Behavior of a Cylindrical Shell under Axial Compression when the Buckling Load has been Exceeded," Rand M 2190, British Aero, Res. Comm., 1942.
D.M.A. Leggett, “The buckling of a long curved panel under axial compression”, HM Stationery Office, Reports and Memorandum No. 1899, Ministry of Aviation, ARC, 1942
D.M.A. Leggett, “The initial buckling of slightly curved panels under combined shear and compression, R. & M. No. 1972, British A.R.C., 1943
D.M.A. Leggett, “The buckling of thin cylindrical shells under axial compression”, Publications de L’Institut mathématique, 1953
Leggett, D. M. A,, "The Buckling of Thin Cylindrical Shells under Axial Compression," Aca. Serb. Sci. Publ. Inst. Math., 7, (1954), 47-60.
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