Fully Implicit Discrete-Adjoint Methods for Rotorcraft Applications
Author:
Affiliation:
1. University of Glasgow, Glasgow, Scotland, G12 8QQ, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054006
Reference45 articles.
1. Aerodynamic Sensitivity Theory for Rotary Stability Derivatives
2. Computation of Aircraft Stability Derivatives Using an Automatic Differentiation Adjoint Approach
3. 11. Observations on Efficiency
4. A mathematical view of automatic differentiation
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