High-Fidelity Aero-Structural Design Optimization of a Supersonic Business Jet
Author:
Affiliation:
1. Stanford University
2. NASA Ames
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-1483
Reference20 articles.
1. Sensitivity Analysis of Discrete Structural Systems
2. 5P. E. Gill, W. Murray, M. A. Saunders, and M. H. Wright. User’s Guide for NPSOL (version 4.0). A FORTRAN Package Nonlinear Programming. Technical Report SOL86-2, Stanford University, Departmentof Operations Research,1986.
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