1. Optimum design of laminated fibre composite plates;Schmidt;Int. J. Numer. Meth. Engng,1977
2. Minimum-weight designs for hat-stiffened composite panels under uniaxial compression;Argarwal;NASA TN D-7779,1974
3. Minimum mass design of filamentary composite panels under combined loads: design based on simplified buckling equations;Stroud;NASA TN D-8257,1976
4. Buckling and vibration of anisotropic or isotropic plate assemblies under combined loadings;Wittrick;Int. J. Mech. Sci.,1974
5. Design and analysis of a stiffened composite fuselage panel;Dickson;NASA CR-159302,1980