Modeling Subscale Rotor Wake in Ground Effect with Accurate Turbulent Length Scales-Reference-Cited by-同舟云学术

Modeling Subscale Rotor Wake in Ground Effect with Accurate Turbulent Length Scales

Published:2017-09 Issue:9 Volume:55 Page:3085-3094
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Kalra Tarandeep S.¹,Baeder James D.¹

Affiliation:

1. University of Maryland, College Park, Maryland 20742

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J055647

Reference21 articles.

1. MilluzzoJ. “Effect of Blade Tip Shape on Rotor In-Ground-Effect Aerodynamics,” Masters Dissertation, Dept. of Aerospace Engineering, Univ. of Maryland, College Park, MD, 2011.

2. NathanN. D. “The Rotor Wake in Ground Effect and its Investigation in a Wind Tunnel,” Ph.D. Dissertation, Dept. of Aerospace Engineering, Univ. of Glasgow, Glasgow, 2010.

3. Effects of Model Scaling on Sediment Transport in Brownout

4. Modeling of Bombardment Ejections in the Rotorcraft Brownout Problem

5. Vorticity Confinement and Advanced Rendering to Compute and Visualize Complex Flows

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