A quantitative study of shape effect on the constant moment plate-bending element of Morley is presented. The so-called eccentricity coefficients were used to express in a very simple form the shape functions and the stiffness matrix of this triangular finite element. Eigenvalues of different shapes of triangles were calculated and the result of this study reaffirms the influence of the smallest triangle angle on the numerical deterioration of the element's properties.
ABDALLA, H., & HASSAN, K. (1985). STUDIES ON THE PLATE-BENDING ELEMENT OF MORLEY. International Conference on Aerospace Sciences and Aviation Technology, 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO), 463-472. doi: 10.21608/asat.1985.26524
MLA
HAMED ABDALLA; KAMAL HASSAN. "STUDIES ON THE PLATE-BENDING ELEMENT OF MORLEY". International Conference on Aerospace Sciences and Aviation Technology, 1, A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO, 1985, 463-472. doi: 10.21608/asat.1985.26524
HARVARD
ABDALLA, H., HASSAN, K. (1985). 'STUDIES ON THE PLATE-BENDING ELEMENT OF MORLEY', International Conference on Aerospace Sciences and Aviation Technology, 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO), pp. 463-472. doi: 10.21608/asat.1985.26524
VANCOUVER
ABDALLA, H., HASSAN, K. STUDIES ON THE PLATE-BENDING ELEMENT OF MORLEY. International Conference on Aerospace Sciences and Aviation Technology, 1985; 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO): 463-472. doi: 10.21608/asat.1985.26524
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