Aerodynamic shape optimization of hovering rotor blades using a coupled free wake–CFD and adjoint method-Reference-Cited by-同舟云学术

Aerodynamic shape optimization of hovering rotor blades using a coupled free wake–CFD and adjoint method

Published:2013-07 Issue:1 Volume:28 Page:21-30
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Farrokhfal H.,Pishevar A.R.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference25 articles.

1. Euler calculation for flow field of a helicopter rotor in hover;Agarwal;J. Aircr.,1987

2. Aerodynamic shape optimization of hovering rotors using compressible CFD;Allen;Aeronaut. J.,2011

3. CFD-based optimization of hovering rotors using radial basis functions for shape parameterization and mess deformation;Allen;Optim. Eng.,2012

4. Computational-fluid-dynamics based twist optimization of hovering rotors;Allen;J. Aircr.,2010

5. D.B. Bliss, T.R. Quackenbush, A.J. Bilanin, A new methodology for helicopter free wake analysis, Presented at the 39th Annual Forum of American Helicopter Society, May 1983, Paper No. A-83-39-75-000.

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