Design Refinement and Performance Analysis of Two-Stage Fan for Small Turbofan Engines-Reference-Cited by-同舟云学术

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Design Refinement and Performance Analysis of Two-Stage Fan for Small Turbofan Engines

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Masud Jehanzeb¹,Ahmed Sijal¹

Affiliation:

1. National University of Sciences & Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-23

Reference9 articles.

1. Blading Aerodynamics Design Optimization With Mechanical and Aeromechanical Constraints

2. 5Cumpsty,N.A.,CompressorAerodynamics,LongmanScientific&Technical,Essex,UK1989.

Cited by 4 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. Flow Field and Performance Evaluation of an Integrated Fan Stage of a Low Bypass Turbofan Engine;AIAA SCITECH 2022 Forum;2022-01-03

2. Design Refinement and Performance Evaluation of a Fan Stage of a Low Bypass Turbofan Engine;AIAA SCITECH 2022 Forum;2022-01-03

3. Advanced Materials and Technologies for Compressor Blades of Small Turbofan Engines;Aerospace;2020-12-22

4. Effect of Casing Recess and Tip Clearance on the Efficiency of High Pressure Turbine Stage with Contoured Endwall NGV;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

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