Aerodynamic shape optimization of hovering rotor blades using a nonlinear frequency domain approach
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Publication:365545
DOI10.1016/J.COMPFLUID.2011.06.014zbMATH Open1271.76300OpenAlexW2157748007MaRDI QIDQ365545
Charles A. Tatossian, Siva K. Nadarajah, Patrice Castonguay
Publication date: 4 September 2013
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: http://www.sciencedirect.com/science/article/pii/S0045793011002027
Cites Work
- Convergence studies of the time accurate and non-linear frequency domain methods for optimum shape design
- Flowfield of a lifting rotor in hover - A Navier-Stokes simulation
- The harmonic adjoint approach to unsteady turbomachinery design
- An adjoint‐based design methodology for CFD problems
- S<scp>HAPE</scp> O<scp>PTIMIZATION IN</scp> F<scp>LUID</scp> M<scp>ECHANICS</scp>
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