Application of the Helios Computational Platform to Rotorcraft Flowfields-Reference-Cited by-同舟云学术

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Application of the Helios Computational Platform to Rotorcraft Flowfields

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
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Author:

Sitaraman Jayanarayanan¹,Wissink Andrew²,Sankaran Venketeswaran²,Jayaraman Buvana²,Datta Anubhav²,Yang Zhi³,Mavriplis Dimitri³,Saberi Hossein⁴,Potsdam Mark⁵,O'Brien David⁶,Cheng Rui⁷,Hariharan Nathan⁸,Strawn Roger⁹

Affiliation:

1. National Institute of Aerospace

2. NASA Ames Research Center

3. University of Wyoming

4. Advanced Rotorcraft Technologies

5. NASA Ames Research Field

6. US Army/AED

7. Advanced Rotocraft Technology, Inc.

8. CREATE-AV

9. US Army/AFDD Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1230

Reference54 articles.

1. A Multi-Code Python-Based Infrastructure for Overset CFD with Adaptive Cartesian Grids

2. Recent enhancements to OVERFLOW

3. CFD Approaches for Simulation of Wing-Body Stage Separation

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4. Enhancing the Resolution of Blade Tip Vortices in Hover with High-Order WENO Scheme and Hybrid RANS–LES Methods;Aerospace;2023-03-08

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