Time accurate unsteady simulation of the stall inception process in the compression system of a US army helicopter gas turbine engine-Reference-Cited by-同舟云学术

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Time accurate unsteady simulation of the stall inception process in the compression system of a US army helicopter gas turbine engine

Published:2004 Issue: Volume: Page:
ISSN:
Container-title:2004 Users Group Conference (DOD_UGC'04)
language:
Short-container-title:

Author:

Hathaway M.D.,Herrick G.,Chen J.,Webster R.

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx5/9724/30702/01420867.pdf?arnumber=1420867

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. Prediction of Sand Transport and Deposition in a Two-Pass Internal Cooling Duct;Journal of Engineering for Gas Turbines and Power;2016-02-17

2. URANS analysis of the effect of realistic inlet distortions on the stall inception of a centrifugal compressor;Computers & Fluids;2015-08

3. Large Eddy Simulation for a Deep Surge Cycle in a High-Speed Centrifugal Compressor With Vaned Diffuser;Journal of Turbomachinery;2015-06-23

4. Prediction of the unsteady turbulent flow in an axial compressor stage. Part 1: Comparison of unsteady RANS and LES with experiments;Computers & Fluids;2015-01

5. Sand transport in a two pass internal cooling duct with rib turbulators;International Journal of Heat and Fluid Flow;2014-04

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