Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers
- 1 May 1999
- journal article
- Published by Elsevier in Computers & Fluids
- Vol. 28 (4-5), 675-700
- https://doi.org/10.1016/s0045-7930(98)00050-4
Abstract
No abstract availableThis publication has 34 references indexed in Scilit:
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