Add to ORKGThe state of the art of automated structural design through the use of optimality criteria, with emphasis on aerospace applications is reviewed. Constraints on stresses, displacements, and buckling strengths under static loading, as well as lower bound limits on natural frequencies and flutter speeds are presented. It is presumed that the reader is experienced in finite element methods of analysis, but is not familiar with optimal design techniques
A method for the optimization of structures to satisfy flutter velocity constraints is presented alo...
A finite-element based procedure is described for obtaining minimum mass designs of structures subje...
Mitchell strain criterion for minimum weight structures using mathematical model
A generalized optimality criterion method consisting of a dual problem solver combined with a compou...
In the design of spacecraft structures, fine tuning the structure to achieve minimum weight with nat...
The results of numerical experiments designed to illustrate how the minimum weight design, accuracy,...
Optimal control models for design of structures with weights minimized by constraints involving fixe...
The rational use of optimality criteria was investigated for a class of structural synthesis problem...
Research carried out is grouped under two topics: (1) Design Optimization, and (2) Integrated Force ...
Dynamic response in current structural problems using computer programs and coordinate transformatio...
A method is presented for configuration optimization of finite element structures, given a reasonabl...
Optimal structural weight in design based on reliability analysis and proof-load test
An approach is presented for determining the minimum weight design of aircraft wing models which tak...
The automated optimum design of airplane wing structures subjected to multiple behavior constraints ...
A numerical procedure was developed for minimizing the structural mass of an aircraft structure whic...
A method for the optimization of structures to satisfy flutter velocity constraints is presented alo...
A finite-element based procedure is described for obtaining minimum mass designs of structures subje...
Mitchell strain criterion for minimum weight structures using mathematical model
A generalized optimality criterion method consisting of a dual problem solver combined with a compou...
In the design of spacecraft structures, fine tuning the structure to achieve minimum weight with nat...
The results of numerical experiments designed to illustrate how the minimum weight design, accuracy,...
Optimal control models for design of structures with weights minimized by constraints involving fixe...
The rational use of optimality criteria was investigated for a class of structural synthesis problem...
Research carried out is grouped under two topics: (1) Design Optimization, and (2) Integrated Force ...
Dynamic response in current structural problems using computer programs and coordinate transformatio...
A method is presented for configuration optimization of finite element structures, given a reasonabl...
Optimal structural weight in design based on reliability analysis and proof-load test
An approach is presented for determining the minimum weight design of aircraft wing models which tak...
The automated optimum design of airplane wing structures subjected to multiple behavior constraints ...
A numerical procedure was developed for minimizing the structural mass of an aircraft structure whic...
A method for the optimization of structures to satisfy flutter velocity constraints is presented alo...
A finite-element based procedure is described for obtaining minimum mass designs of structures subje...
Mitchell strain criterion for minimum weight structures using mathematical model