FULL-LENGTH PAPERS - Aerodynamic Optimization of Turbomachinery Cascades Using Euler-Boundary-Layer Coupled Genetic Algorithms
Journal of propulsion and power ; 18 , 3
2002
Aufsatz (Zeitschrift)
Unbekannt
FULL-LENGTH PAPERS - Missile Aerodynamic Shape Optimization Using Genetic Algorithms
Online Contents | 2000
|A 3D Compressible Euler Solver for Turbomachinery Cascades
British Library Conference Proceedings | 1994
|