Development of an advanced vaneless inlet particle separator for helicopter engines-Reference-Cited by-同舟云学术

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Development of an advanced vaneless inlet particle separator for helicopter engines

Published:1985-07-08 Issue: Volume: Page:
ISSN:
Container-title:21st Joint Propulsion Conference
language:
Short-container-title:

Author:

VITTAL B.¹,TIPTON D.¹,BENNETT W.¹

Affiliation:

1. General Motors Corp.,Allison Gas Turbine Div., Indianapolis, IN

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1985-1277

Reference12 articles.

1. Shieh, C. F., Delaney, R. A., and Tipton, D. L. "Analysis of the Flow Field in an Engine Inlet Particle Separator," Computationof Internal Flows: Methods and Applications, ASME publication FED-Vol 14,1984. w

2. Hamed, A. "Particle Dynamics of Inlet Flow Fields with Swirling Vanes," AIAA paper No. 81-0001,1981.

3. Denton J. D. "An Improved Time Marching Method for Turbomachinery Calculation,'' ASME paper 82-GT-239, 1982.

Cited by 3 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. Numerical study of internal flow field and flow passage improvement of an inlet particle separator;Frontiers in Energy;2011-09-23

2. Computer simulation of water ingestion for the T800-LHT-801 engine anti-icing test inlet;32nd Joint Propulsion Conference and Exhibit;1996-07-01

3. Particle dynamics simulations in inlet separator with an experimentally based bounce model;29th Joint Propulsion Conference and Exhibit;1993-06-28

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