Multipoint aerodynamic wing optimization in viscous flow

Journal of Aircraft

Volumn 38, Issue 5, 2001, Pages 860-867

  Szmelter, J ^a  

^a CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; BOUNDARY LAYERS; CONTROL THEORY; NAVIER STOKES EQUATIONS; OPTIMIZATION; VISCOUS FLOW; WINGS;

EULER EQUATIONS;

AERODYNAMICS;

EID: 0035438703     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2845     Document Type: Article

References (26)

1. Optimum aerodynamic design via boundary control
2. Optimum aerodynamic design using CFD and control theory
3. Aerodynamic shape optimisation of wing and wing-body configurations using control theory
4. Aerodynamic design via control theory
5. Control theory based airfoil design using the euler equations
6. Optimum aerodynamic design using the navier-stokes equations
7. Aerodynamic shape optimisation of complex aircraft configurations via an adjoint formulation
8. Three-dimensional aerodynamic shape optimisation of wings using sensitivity analysis
9. Business jet wing design using aerodynamic shape optimisation
10. Optimal shape design for aerodynamics
11. Aerodynamic design optimisation using sensitivity analysis and computational fluid dynamics
12. Three-dimensional aerodynamic shape optimisation using genetic evolution and gradient search
13. Viscous coupling techniques using unstructured and multiblock meshes
14. Solution of the euler equations by a multigrid method
15. Transonic flow calculation for aircraft
16. Multigrid algorithms for compressible flow calculations
17. The analogy between streamline curvature and buoyancy in turbulent shear flow
18. The prediction of turbulent boundary layer development in compressible flow
19. Vicsous-inviscid calculation on high lift separated compressible flow over airfoils and wings
20. Pressure distributions on research wing W4 mounted on an axisymmetric body, Case B3