Application of sweep to improve the efficiency of a transonic fan. I

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Application of sweep to improve the efficiency of a transonic fan. I - Design

Published:1995-01 Issue:1 Volume:11 Page:49-54
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Neubert R. J.¹,Hobbs D. E.¹,Weingold H. D.¹

Affiliation:

1. Pratt and Whitney, United Technologies, East Hartford, Connecticut 06108

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.23839

Reference12 articles.

Cited by 8 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 investigation and modeling of sweep effects on inlet flow field of axial compressor cascades;Chinese Journal of Aeronautics;2024-02

2. Experimental and Numerical Investigations of Inlet Circumferential Fluctuations in Swept Compressor Cascades;Journal of Aerospace Engineering;2023-09

3. Investigating the aerodynamic design of a novel tandem fan with a partial-span booster rotor;Aerospace Science and Technology;2023-01

4. Aerodynamics of Sweep in a Tandem-Bladed Subsonic Axial Compressor Rotor;Journal of Fluids Engineering;2022-08-08

5. Investigations on low speed axial compressor with forward and backward sweep;Journal of Thermal Science;2007-05

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