Dependence of optimal structural weight on aerodynamic shape for a High Speed Civil Transport
- 22 August 1996
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Developing customized weight function by structural optimization on parallel computersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Certification of a CFD code for high-speed civil transport design optimizationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Multidisciplinary aerospace design optimization - Survey of recent developmentsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Variable-complexity response surface approximations for wing structural weight in HSCT designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Variable-complexity response surface aerodynamic design of an HSCT wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Multidisciplinary optimization of the high-speed civil transportPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Supersonic transport wing minimum weight design integrating aerodynamics and structuresJournal of Aircraft, 1994
- Variable-complexity aerodynamic optimization of a high-speed civil transport wingJournal of Aircraft, 1994
- Aerodynamic optimization of an HSCT configuration using variable-complexity modelingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Factorial Designs, the |X′X| Criterion, and Some Related MattersTechnometrics, 1971