Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers

被引：0

作者：

Reuther, J. ^{[1
]}

Alonso, J.J. ^{[2
]}

Rimlinger, M.J. ^{[3
]}

Jameson, A. ^{[2
]}

机构：

[1] MCAT Institute, NASA Ames Research Center, MS 227-6, Moffett Field, CA 94035, United States

[2] Dept. of Aero. Andw Astronautics, Stanford University, Stanford, CA 94305, United States

[3] Simco, NASA Ames Research Center, MS 227-6, Moffett Field, CA 94035, United States

来源：

Computers and Fluids | / 28卷 / 4-5期

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页码：675 / 700