ADjoint: An Approach for the Rapid Development of Discrete Adjoint Solvers
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.29123
Reference41 articles.
1. On optimum design in fluid mechanics
2. Aerodynamic design via control theory
3. Numerical Aerodynamic Optimization Incorporating Laminar-Turbulent Transition Prediction
4. Multipoint and Multi-Objective Aerodynamic Shape Optimization
5. Constrained Multipoint Aerodynamic Shape Optimization Using an Adjoint Formulation and Parallel Computers, Part 1
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