A general-purpose optimization tool for multidisciplinary applications, whi
ch in the literature is known as COMETBOARDS, is bring developed at NASA Le
wis Research Center. The modular organization of COMETBOARDS includes sever
al analyzers and state-of-the-art optimization algorithms along with their
cascading strategy. The code structure allows quick integration of new anal
yzers and optimizers. The COMETBOARDS code reads input information from a n
umber of data files, formulates a design as a set of multidisciplinary nonl
inear programming problems, and then solves the resulting problems. COMETBO
ARDS can be used to solve a large problem, which can be defined through mul
tiple disciplines, each of which can be further broken down into several su
bproblems. Alternatively, a small portion of a large problem can be optimiz
ed in an effort to improve an existing system. Some of the other unique fea
tures of COMETBOARDS include design variable formulation, constraint formul
ation, subproblem coupling strategy, global scaling technique, analysis app
roximation, use of either sequential or parallel computational modes, and s
o forth. The special features and unique strengths of COMETBOARDS assist co
nvergence and reduce the amount of CPU time used to solve the difficult opt
imization problems of aerospace industries. COMETBOARDS has been successful
ly used to solve a number of problems, including structural design of space
station components, design of nozzle components of an air-breathing engine
, configuration design of subsonic and supersonic aircraft, mixed flow turb
ofan engines, wave rotor topped engines, and so forth. This paper introduce
s the COMETBOARDS design tool and its versatility, which is illustrated by
citing examples from structures, aircraft design, and air-breathing propuls
ion engine design. (C) 2000 Elsevier Science Ltd. All rights reserved.