Integration- and Intake-Induced Flow Distortions and Their Impact on Aerodynamic Fan Performance-Reference-Cited by-同舟云学术

Integration- and Intake-Induced Flow Distortions and Their Impact on Aerodynamic Fan Performance

Published:2015-07-10 Issue: Volume: Page:251-269
ISSN:1612-2909
Container-title:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
language:
Short-container-title:

Author:

Schnell Rainer,Schönweitz Dirk,Theune Marius,Corroyer Johakim

Publisher

Springer International Publishing

Link

http://link.springer.com/content/pdf/10.1007/978-3-319-21127-5_15

Reference37 articles.

1. ARP1420, SAE Gas Turbine Engine Inlet Flow Distortion Guidelines, Society of Automotive Engineers, Warrendale (2002)

2. Albers, J., Miller, B.: Effect of Subsonic Inlet Lip Geometry on Predicted Surface and Flow Mach Number Distribution, NASA Technical Note TN-D-7446, December 1973

3. Albert, M., Bestle, D.: Aerodynamic Optimization of Nacelle and Intake, ASME Paper GT2013-94857, ASME Turbo Expo 2013 San Antonio/Texas (2013)

4. Aulich, A.-L., Goerke, D., Blocher, M., Nicke, E., Kocian, F.: Automated Optimization Strategy on a Counter Rotating Fan, ASME Paper GT2013-94259, ASME Turbo Expo San Antonio/US (2013)

5. Becker, R.-G., Wolters, F., Nauroz, M., Otten, T.: Development of a gas turbine performance code and its application to preliminary engine design, DLRK2013-241485, Proceedings of the German Aerospace Congress, September 27–29, Bremen/Germany (2011)

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. A review of installation effects of ultra-high bypass ratio engines;Progress in Aerospace Sciences;2020-11

2. Full Annulus Simulations of a Transonic Axial Compressor Stage with Distorted Inflow at Transonic and Subsonic Blade Tip Speed;International Journal of Turbomachinery, Propulsion and Power;2018-02-14

3. Aerodynamic Performance Characteristics of the Installed V2527 Fan at Ground Operation;54th AIAA Aerospace Sciences Meeting;2016-01-02