Recent experiments on vortex collisions with a cylinder-Reference-Cited by-同舟云学术

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Recent experiments on vortex collisions with a cylinder

Published:1995-06-19 Issue: Volume: Page:
ISSN:
Container-title:Fluid Dynamics Conference
language:
Short-container-title:

Author:

Mahalingam R,Peterson K,Funk R,Komerath N,Conlisk A

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-2236

Reference11 articles.

1. Interactional Aerodynamics—A New Challenge to Helicopter Technology

2. The core is initially flattened by the passage of the rotor blade pressure distribution, and then recovers to itscircularshape. Airloads,M.LT. Aeroel.8mc.Res. Lab. Report, ASRL TR 178-1,March '75.

3. Egolf, T.A., and Landgrebe, A.J. "Helicopter RotorWakeGeometryandItsInfluenceinForward Flight".NASACR 3726,October 1983.

4. Lorber,P.F., and Egolf, T.A. "An Unsteady Helicopter Rotor-Fuselage Interaction Analysis", NASA CR4178,1988.

Cited by 2 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. Use of a deformable core vortex model in predicting vortex-surface interaction;37th Aerospace Sciences Meeting and Exhibit;1999-01-11

2. Modeling of the collision of a rotor-tip vortex with an airframe;35th Aerospace Sciences Meeting and Exhibit;1997-01-06

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