CFD- and CSD-Based Aeroelastic Computations of Helicopter Rotor Blades Using a Modular Approach-Reference-Cited by-同舟云学术

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CFD- and CSD-Based Aeroelastic Computations of Helicopter Rotor Blades Using a Modular Approach

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA Fluid Dynamics Conference
language:
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Author:

Guruswamy GP¹

Affiliation:

1. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-4199

Reference38 articles.

1. Anon.RCASTheoryManual,Version2.0.TechnicalReportUSAMCOM/AFDD TR02-A-005,US ArmyAviationandMissileCommand,Moffett Field,CA, June 2000.

2. Johnson,W.RecentDevelopmentsinRotaryWingAerodynamicTheory,‖ AIAA Journal,Vol.24,No8,1986,pp.1219-1244.

3. Ballhaus,W.F.and Bridgeman,J .O.Numerical SolutionTechniquesfor UnsteadyTransonicproblems,‖AGARDRepNo 679,PaperNO16(1980).

Cited by 1 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. Dynamic Mesh Analyses of Helicopter Rotor–Fuselage Flow Interaction in Forward Flight;Journal of Aerospace Engineering;2016-11

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