Unsteady Euler algorithm with unstructured dynamic mesh for complex-aircraft aeroelastic analysis
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-1189
Reference13 articles.
1. Calculation of Inviscid Transonic Flow over a Complete Aircraft
2. . vOI. 24, 1987, pp.1741-1756.
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