Helicopter fuselage drag prediction - State of the art in Europe-Reference-Cited by-同舟云学术

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Helicopter fuselage drag prediction - State of the art in Europe

Published:2001-01-08 Issue: Volume: Page:
ISSN:
Container-title:39th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Gleize V.¹,Costes M.¹,von Gehr H.²,Renzoni P.³,Amato M.³,Kokkalis A.⁴,Mottura L.⁵,Serr C.⁶,Larrey E.⁷,Filippone A.⁸

Affiliation:

1. ONERA, Chatillon, France

2. DLR, Stuttgart, Germany

3. CIRA, Capua, Italy

4. GKN Westland Helicopters, Ltd., Yeovil, United Kingdom

5. Agusta S.P.A., Samarate, Italy

6. Eurocopter France, Marignane

7. SIMULOG, Guyancourt, France

8. Technical Univ. of Denmark, Lyngby

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-999

Reference21 articles.

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aerodynamic Investigations on a Helicopter Fuselage;29th AIAA Applied Aerodynamics Conference;2011-06-27

2. Aerodynamic Analysis of a Helicopter Fuselage;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2010

3. Low-Mach-Number Preconditioning Applied to Turbulent Helicopter Fuselage Flowfield Computation;AIAA Journal;2003-04

4. Navier–Stokes solvers in European aircraft design;Progress in Aerospace Sciences;2002-11

5. Simulation of the Unsteady Flow Field Around a Complete Helicopter with a Structured RANS Solver;High Performance Computing on Vector Systems

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