Aerodynamic Shape Optimization of Hovering Rotors Using a Discrete Adjoint of the Reynolds-Averaged Navier–Stokes Equations
- 1 July 2011
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 56 (3), 1-11
- https://doi.org/10.4050/jahs.56.032002
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Discrete Adjoint-Based Design Optimization of Unsteady Turbulent Flows on Dynamic Unstructured GridsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2009
- Helicopter Rotor Design Using a Time-Spectral and Adjoint-Based MethodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2008
- Sensitivity Analysis Using Direct Differentiation and Adjoint Vector Methods for Helicopter Rotor Flow In HoverPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2008
- Status of the elsA Software for Flow Simulation and Multi-Disciplinary ApplicationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2008
- Numerical optimization of helicopter rotor aerodynamic performance in hoverAerospace Science and Technology, 2005
- 2D and 3D aerodynamic shape optimisation using the adjoint approachAerospace Science and Technology, 2004
- Navier-Stokes Prediction of Helicopter Rotor Performance in Hover Including Aeroelastic EffectsJournal of the American Helicopter Society, 2001
- Computational fluid dynamics for aerodynamic design - Its current and future impactPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2001
- Resolving the Dependence on Freestream Values for the k- Turbulence ModelAIAA Journal, 2000
- Two-equation eddy-viscosity turbulence models for engineering applicationsAIAA Journal, 1994