Parallel Adaptive Finite Element Euler Flow Solver for Rotary Wing Aerodynamics
- 1 June 1997
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 35 (6), 937-944
- https://doi.org/10.2514/2.187
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
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