High-Fidelity Aerostructural Gradient Computation Techniques with Application to a Realistic Wing Sizing
Author:
Affiliation:
1. ONERA – Paris Saclay University, F-92322 Châtillon, France
2. CNAM, National Conservatory of Arts and Crafts, 2 rue Conté, 75003 Paris, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056736
Reference36 articles.
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2. HicksR. M.SzelazekC. A. “Airfoil Design by Numerical Optimization Using a Minicomputer,” NASA TM 78502, 1978.
3. BarthelemyJ.F. M.BergenF. “Shape Sensitivity Analysis of Wing Static Aeroelastic Characteristics,” NASA TP 2808, 1988.
4. Aeroelastic tailoring - Theory, practice, and promise
5. Integrated aerodynamic/structural design of a sailplane wing
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