Efficient identification of critical stresses in structures subject to dynamic loads

Optimum structural design problems generally employ constraints which are parametric in terms of space and time variables. A parametric constraint may be replaced by equivalent critical point constraints at its local minima for optimization applications. In complex structures, accurate identification of such critical points is computationally expensive due to the cost of finite element analyses. Three techniques are described for efficiently and accurately identifying critical points for space- and time-dependent parametric constraints. An adaptive search technique and a spline interpolation technique are developed for exactly known response. A least squares spline approximation is suggested for noisy behavior. A helicopter tail-boom structure subjected to transient loading is used as an example to demonstrate the techniques described. All three techniques are shown to be computationally efficient for critical point identification and the least squares approximation also removes noise from the data. The case of multiple constraints per element is shown to be particularly suited to the use of spline techniques.

[1]  R. Haftka,et al.  Approximation methods for combined thermal/structural design , 1979 .

[2]  Emilio Rosenblueth Optimum Design to Resist Earthquakes , 1979 .

[3]  W. A. Thornton,et al.  Structural synthesis of an ablating thermostructural panel. , 1968 .

[4]  C. D. Mote,et al.  Optimization methods for engineering design , 1971 .

[5]  L. Schmit,et al.  Some Approximation Concepts for Structural Synthesis , 1974 .

[6]  Raymond M. Brach,et al.  Minimum dynamic response for a class of simply supported beam shapes , 1968 .

[7]  Lucien A. Schmit,et al.  Optimum Structural Design with Dynamic Constraints , 1976 .

[8]  Edward J. Haug,et al.  Optimal structural design under dynamic loads , 1977 .

[9]  R. Brach Optimum Design of Beams for Sudden Loading , 1968 .

[10]  Howard M. Adelman,et al.  Preliminary Design Procedure for Insulated Structures Subjected to Transient Heating. , 1979 .

[11]  Raphael T. Haftka,et al.  Parametric Constraints with Application to Optimization for Flutter Using a Continuous Flutter Constraint , 1975 .

[12]  Walter D. Pilkey,et al.  OPTIMUM SHOCK AND VIBRATION ISOLATION , 1971 .

[13]  L. Watson,et al.  Design-oriented identification of critical times in transient response , 1986 .

[14]  L. A. Schmit,et al.  Structural optimization with dynamic behavior constraints , 1985 .

[15]  M. P. Kapoor Automated optimum design of structures under dynamic response restrictions , 1969 .

[16]  Hiroshi Yamakawa,et al.  Optimum Structural Designs in Dynamic Response , 1981 .

[17]  K. D. Willmert,et al.  Optimum Design of a Linear Multi-Degree-of-Freedom Shock Isolation System , 1972 .

[18]  R. L. Fox,et al.  Structural optimization in the dynamics response regime - A computational approach , 1970 .

[19]  E. J. Haug,et al.  Sensitivity Analysis and Optimization of Structures for Dynamic Response , 1978 .

[20]  Henry N. Christiansen,et al.  Synthesis of A Space Truss Based on Dynamic Criteria , 1966 .

[21]  Franklin Y. Cheng,et al.  Nonlinear Optimum Design of Dynamic Damped Frames , 1976 .

[22]  R. W. Mayne,et al.  Optimum Design of an Impact Absorber , 1974 .

[23]  Edward J. Haug,et al.  EFFICIENT TREATMENT OF CONSTRAINTS IN LARGE-SCALE STRUCTURAL OPTIMIZATION. , 1981 .

[24]  J. Cassis,et al.  On implementation of the extended interior penalty function. [optimum structural design] , 1976 .

[25]  Edward J. Haug,et al.  Optimal design of dynamically loaded continuous structures , 1978 .

[26]  W. J. Stroud,et al.  Automated preliminary design of simplified wing structures to satisfy strength and flutter requirements , 1972 .

[27]  B. Kato,et al.  Optimum Earthquake Design of Shear Buildings , 1972 .

[28]  M. P. Kapoor,et al.  Optimum Configuration of Transmission Line Towers in Dynamic Response Regime , 1981 .