An Adjoint-based Aerodynamic Shape Optimization Strategy for Trimmed Aircraft with Active Engines
Author:
Affiliation:
1. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3754
Reference22 articles.
1. 1AIAA Aerodynamic Design Optimization Discussion Group, https://info.aiaa.org/tac/ASG/APATC/AeroDesignOpt-DG/default.aspx, Accessed: 04-20-2017.
2. Aerodynamic Shape Optimization of Common Research Model Wing–Body–Tail Configuration
3. Progress in Aerodynamic Shape Optimization Based on the Reynolds-Averaged Navier-Stokes Equations
4. Gradient-Based Optimization of CRM Wing-alone and Wing-body-tail Configurations by RANS Adjoint Technique
5. Investigations of propulsion integration interference effects on a transport aircraft configuration
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