Computational Fluid Dynamics Modeling of Helicopter Fuselage Drag-Reference-Cited by-同舟云学术

Computational Fluid Dynamics Modeling of Helicopter Fuselage Drag

Published:2015-09 Issue:5 Volume:52 Page:1634-1643
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Batrakov A.¹,Garipova L.¹,Kusyumov A.¹,Mikhailov S.¹,Barakos G.²

Affiliation:

1. Kazan National Research Technical University, 420111, Kazan, Russia

2. School of Engineering, University of Liverpool, Liverpool, England L69 3GH, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033019

Reference19 articles.

1. LeishmanJ. G., Principles of Helicopter Aerodynamics, Cambridge Univ. Press, New York, 2002, p. 496.

2. “Aerodynamic Simulation of a Complete Helicopter Configuration, The Blind Test Activity of the GOAHEAD Project,” Nationaal Lucht- en Ruimtevaartlaboratorium (NLR) Rept. NLR-TP-604, Amsterdam, Dec. 2007.

3. Rotorcraft Fuselage Drag Reduction Using Combustion Powered Actuators

4. Aerodynamic Drag Prediction of Helicopter Fuselage

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