A finite-element based procedure is described for obtaining minimum mass designs of structures subjected to combined thermal and mechanical loading and both strength and thermal constraints. The procedure is based on a mathematical programming method using the Sequence of Unconstrained Minimizations Technique (SUMT) in which design requirements are incorporated by an exterior penalty function. The procedure is limited to steady-state temperatures which are controlled by structural sizing only. The optimization procedure is demonstrated by the design of a structural wing box with both mechanical loading and external heating, subject to design constraints on stress, minimum gage, and temperature. The final design for these conditions is compa...
Aircraft structure subjected to elevated temperature and acoustic loading present a challenging desi...
Thermal stress analyses are an important aspect in the development of aerospace vehicles such as the...
Space shuttle main engine (SSME) blades are subject to severe thermal, pressure, and forced vibratio...
A thermal optimality criterion is presented for sizing members of heated structures with multiple te...
An algorithm is reported for resizing structures subjected to combined thermal and mechanical loadin...
General equations are developed for the design of efficient structures protected from thermal enviro...
The state of the art of automated structural design through the use of optimality criteria, with emp...
An optimization system is described that consists of the finite-element analysis program known as En...
Different finite element models previously set up for thermal analysis of the space shuttle orbiter ...
Three minimizing techniques are evaluated to determine the most efficient method for minimizing the ...
Research carried out is grouped under two topics: (1) Design Optimization, and (2) Integrated Force ...
Research on the optimization of wing structures under multiple constraint such as strength, displace...
A method is presented for configuration optimization of finite element structures, given a reasonabl...
In this paper, we introduce a level set method topology optimization method of structures subjected ...
A modular program for design optimization of thermal protection systems is discussed. Its capabiliti...
Aircraft structure subjected to elevated temperature and acoustic loading present a challenging desi...
Thermal stress analyses are an important aspect in the development of aerospace vehicles such as the...
Space shuttle main engine (SSME) blades are subject to severe thermal, pressure, and forced vibratio...
A thermal optimality criterion is presented for sizing members of heated structures with multiple te...
An algorithm is reported for resizing structures subjected to combined thermal and mechanical loadin...
General equations are developed for the design of efficient structures protected from thermal enviro...
The state of the art of automated structural design through the use of optimality criteria, with emp...
An optimization system is described that consists of the finite-element analysis program known as En...
Different finite element models previously set up for thermal analysis of the space shuttle orbiter ...
Three minimizing techniques are evaluated to determine the most efficient method for minimizing the ...
Research carried out is grouped under two topics: (1) Design Optimization, and (2) Integrated Force ...
Research on the optimization of wing structures under multiple constraint such as strength, displace...
A method is presented for configuration optimization of finite element structures, given a reasonabl...
In this paper, we introduce a level set method topology optimization method of structures subjected ...
A modular program for design optimization of thermal protection systems is discussed. Its capabiliti...
Aircraft structure subjected to elevated temperature and acoustic loading present a challenging desi...
Thermal stress analyses are an important aspect in the development of aerospace vehicles such as the...
Space shuttle main engine (SSME) blades are subject to severe thermal, pressure, and forced vibratio...