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Analysis of Experimental and Numerical Studies of the Rudimentary Landing Gear

  • Published:2011-01-04 Issue: Volume: Page:
  • ISSN:
  • Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
  • language:
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Author:

Spalart Philippe1,Mejia Kevin1

Affiliation:

1. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Reference14 articles.

1. 1Lockard,D.P."SummaryofthetandemcylindersolutionsfromtheBANC-Iworkshop."AIAAPaper2011-

2. A New Version of Detached-eddy Simulation, Resistant to Ambiguous Grid Densities

3. 3https://info.aiaa.org/tac/ASG/FDTC/DG/BECAN_files_/Workshop_June_2010_Final_problem_Statements/Contact_Inform ation.pdf

4. Detached-Eddy Simulations Over a Simplified Landing Gear

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2. Investigation of Rotor Tip Vortex in Hover Based on IDDES Methods;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2019-02

3. Numerical investigation of unsteady flow past rudimentary landing gear using DDES, LES and URANS;Engineering Applications of Computational Fluid Mechanics;2018-01

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