Optimization of Vane-Type Vortex Generators for Tiltrotor Wings using Computational Fluid Dynamics-Reference-Cited by-同舟云学术

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Optimization of Vane-Type Vortex Generators for Tiltrotor Wings using Computational Fluid Dynamics

Published:2016-01-02 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA Aerospace Sciences Meeting
language:
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Author:

Bevan Rhodri¹,Poole Daniel J.¹,Allen Christian B.¹,Rendall T.¹

Affiliation:

1. University of Bristol

Publisher

American Institute of Aeronautics and Astronautics

Reference65 articles.

1. 1M.D. Maisel, D.J. Giulianetti, and D.C. Dugan. The history of the XV-15 tilt rotor research aircraft: From concept to flight. Technical Report SP 2000-4517, NASA, 2000.

2. 2M.D. Weiberg, J.A. Maisel. Wind-tunnel tests of the XV-15 tilt rotor aircraft. Technical Report TM 81177, NASA.

3. Flowfield Measurement of Device-Induced Embedded Streamwise Vortex on a Flat Plate

4. Effect of Midwing Vortex Generators on V-22 Aircraft Forward-Flight Aerodynamics

Cited by 3 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. Numerical investigation of the effects of vortex generators on the Bell A821201 airfoil;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2021-10-29

2. An extension of a strong viscous–inviscid coupling method for modeling the effects of vortex generators;Wind Engineering;2018-06-14

3. The Collaborative Development of New CFD Methods Adapted for Tilt Rotor Aircraft in the HiPerTilt Project;35th AIAA Applied Aerodynamics Conference;2017-06-02

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