Progress towards hybrid RANS-LES modeling for high-speed jet flows-Reference-Cited by-同舟云学术

Progress towards hybrid RANS-LES modeling for high-speed jet flows

Published:2002-01-14 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA Aerospace Sciences Meeting & Exhibit
language:
Short-container-title:

Author:

Arunajatesan S.¹,Kannepalli C.,Dash S.

Affiliation:

1. Combustion Research and Flow Technology, Inc., Dublin, PA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-428

Reference19 articles.

1. Unsteady RANS-LES simulations of cavity flowfields

2. Sinha, N., Hosangadi, A. and Dash, S.M."The CRAFT NS Code and Preliminary Applications to Steady/Unsteady Reacting, Multi-Phase Jet/Plume Flowfield Problems," 19thJANNAF Exhaust Plume TechnologyMeeting,CPIA Pub. 568,May 1991, pp.203-226.

3. Rai,M.M. "Navier Stokes Simulations of Blade Vortex Interaction using High-Order Accurate Upwind Schemes",AIAA-87-0543, 1987.

Cited by 10 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. Comparison of turbulence models for solving problems of swirling jet flows;E3S Web of Conferences;2023

2. Modeling of Turbulence;Internal Combustion Processes of Liquid Rocket Engines;2016-05-20

3. Large eddy simulation applications in gas turbines;Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences;2009-07-28

4. Suppression of Cavity Loads Using Leading-Edge Blowing;AIAA Journal;2009-05

5. Navier–Stokes analysis methods for turbulent jet flows with application to aircraft exhaust nozzles;Progress in Aerospace Sciences;2006-07