Aerodynamic design optimization of helicopter rotor blades including airfoil shape for forward flight-Reference-Cited by-同舟云学术

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Aerodynamic design optimization of helicopter rotor blades including airfoil shape for forward flight

Published:2015-04 Issue: Volume:42 Page:106-117
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Vu N.A.,Lee J.W.

Funder

National Foundation for Science and Technology Development

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. An implicit upwind algorithm for computing turbulent flows on unstructured grids;Anderson;Comput. Fluids,1994

2. Advanced configuration generation technique for the complex aircraft geometry;Azamatov,2008

3. Influence of airfoil on stall flutter boundaries of articulated helicopter rotors;Benson,1972

4. Airfoil design and rotorcraft performance;Bousman,2002

5. Flight testing the UH-60A airloads aircraft;Bousman,1994

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3. Multifidelity aerodynamic shape optimization for airfoil dynamic stall mitigation using manifold mapping;Journal of Computational Science;2024-01

4. Compact and Intuitive Airfoil Parameterization Using a Physics-Aware Variational Autoencoder;2024

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