Control theory based airfoil design using the Euler equationsA. Jameson, Josephine Reuther|5th Symposium on Multidisciplinary Analysis and Optimization|1994Cited by 157
Aerodynamic shape optimization of wing and wing-body configurations using control theoryJosephine Reuther, A. Jameson|33rd Aerospace Sciences Meeting and Exhibit|1995Cited by 104
Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computersJosephine Reuther, A. Jameson, Juan J. Alonso et al.|Computers & Fluids|1999Cited by 90
Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computersJosephine Reuther, A. Jameson, Juan J. Alonso et al.|35th Aerospace Sciences Meeting and Exhibit|1997Cited by 76
An efficient multiblock method for aerodynamic analysis and design on distributed memory systemsJuan J. Alonso, John Vassberg, A. Jameson et al.|13th Computational Fluid Dynamics Conference|1997Cited by 43