High-Fidelity Aero-Structural Design Using a Parametric CAD-Based Model
Author:
Affiliation:
1. Stanford University
2. UTIAS
3. NASA Ames Research Center
4. MIT
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-3429
Reference20 articles.
1. Sensitivity Analysis of Discrete Structural Systems
2. 4P. 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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