Development of the quasi-procedural method for use in aircraft configuration optimization
- 17 August 1992
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Structural optimization for joined-wing synthesisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Variable-complexity aerodynamic optimization of an HSCT wing using structural wing-weight equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Design synthesis and optimization of joined-wing transportsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- A quasi-procedural, knowledge-based system for aircraft designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- User's Guide for NPSOL (Version 4.0): A Fortran Package for Nonlinear Programming.Published by Defense Technical Information Center (DTIC) ,1986
- Airplane engine selection by optimization on surface fit approximationsJournal of Aircraft, 1975