Scalable Parallel Approach for High-Fidelity Steady-State Aeroelastic Analysis and Adjoint Derivative Computations

Title
Scalable Parallel Approach for High-Fidelity Steady-State Aeroelastic Analysis and Adjoint Derivative Computations
Authors
Keywords
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Journal
AIAA JOURNAL
Volume 52, Issue 5, Pages 935-951
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2014-03-13
DOI
10.2514/1.j052255

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