Applications to fixed-wing aircraft and spacecraft

Aerospace-industry applications of general-purpose structural optimization codes have not progressed as far as they might due to the lack of preprocessor capabilities. With the emergence of a new generation of graphic preprocessors that are capable of creating design models, these methods will gain acceptance. Attention is given to recent innovative applications of the Flutter and Strength Optimization Program and TSO, and the role of structural optimization in a multidisciplinary design system. Illustrative aircraft structure examples are used throughout the presentation.

[1]  Robert C. Scott,et al.  A Taguchi study of the aeroelastic tailoring design process , 1991 .

[2]  G. N. Vanderplaats,et al.  ADS-1 - A new general-purpose optimization program. [automated design synthesis] , 1984 .

[3]  J. S. Reaser,et al.  Study for the optimization of a transport aircraft wing for maximum fuel efficiency. Volume 1: Methodology, criteria, aeroelastic model definition and results , 1985 .

[4]  Tze Hsin Woo,et al.  Space frame optimization subject to frequency constraints , 1987 .

[5]  H. Ide,et al.  Optimization of nonlinear aeroelastic tailoring criteria , 1988 .

[6]  Augustine R. Dovi,et al.  Multilevel Decomposition Approach to the Preliminary Sizing of a Transport Aircraft Wing , 1988 .

[7]  Jaroslaw Sobieszczanskisobieski,et al.  On the sensitivity of complex, internally coupled systems , 1988 .

[8]  T. R. Bement,et al.  Taguchi techniques for quality engineering , 1995 .

[9]  Edwin Lerner,et al.  Applications of integrated design/analysis systems in aerospace structural design , 1989 .

[10]  F. Abdi,et al.  The art of spacecraft design: A multidisciplinary challenge , 1989 .

[11]  Garret N. Vanderplaats,et al.  COPES - A Fortran Control Program for Engineering Synthesis. , 1982 .

[12]  Jr. N. Krone Divergence elimination with advanced composites , 1975 .

[13]  Michael Love,et al.  Aeroelastic tailoring in vehicle design synthesis , 1991 .

[14]  L. Austel,et al.  An approach to an aero/thermal/elastic design system , 1988 .

[15]  K. M. Riley,et al.  Sensitivity of Optimum Solutions of Problem Parameters , 1982 .

[16]  Tze Woo,et al.  Structural optimization of large spacecraft , 1992 .

[17]  G. L. Giles,et al.  Multidisciplinary optimization applied to a transport aircraft , 1984 .

[18]  J. L. Walsh,et al.  Application of mathematical optimization procedures to a structural model of a large finite-element wing , 1986 .

[19]  Holt Ashley,et al.  On Making Things the Best-Aeronautical Uses of Optimization , 1982 .

[20]  T. Wilson,et al.  Automated structural analysis for hypersonic vehicles , 1990 .