The role of fiber and matrix in crash energy absorption of composite materials
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[1] L. A. Schmit,et al. NEWSUMT: A FORTRAN program for inequality constrained function minimization, users guide , 1979 .
[2] W. Johnson,et al. Recent developments in the dynamics of advanced rotor systems , 1985 .
[3] R. B. Taylor,et al. Helicopter Vibration Reduction by Rotor Blade Modal Shaping , 1982 .
[4] Peretz P. Friedmann,et al. Optimum design of rotor blades for vibration reduction in forward flight , 1984 .
[5] Hirokazu Miura,et al. Applications of numerical optimization methods to helicopter design problems: A survey , 1984 .
[6] Garret N. Vanderplaats,et al. CONMIN: A FORTRAN program for constrained function minimization: User's manual , 1973 .
[7] Inderjit Chopra,et al. Design sensitivity analysis for an aeroelastic optimization of a helicopter blade , 1987 .
[8] David A. Peters,et al. Design of helicopter rotor blades for optimum dynamic characteristics , 1986 .
[9] C. D. Mote,et al. Optimization methods for engineering design , 1971 .
[10] Peretz P. Friedmann,et al. Formulation and solution of rotary-wing aeroelastic stability and response problems , 1983 .
[11] Peretz P. Friedmann,et al. Application of modern structural optimization to vibration reduction in rotorcraft , 1984 .