Radical Guide Vane Design and Optimization-Reference-Cited by-同舟云学术

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Radical Guide Vane Design and Optimization

Published:2018-11 Issue:6 Volume:34 Page:1455-1466
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Rife Max E.¹,Barbarossa Fernando²,di Mare Luca³,Parry Anthony B.⁴,Green Jeffrey S.⁵

Affiliation:

1. University of Oxford, Oxford, England OX2 0ES, United Kingdom

2. Imperial College London, London, England SW7 2BX, United Kingdom

3. St. John’s College, University of Oxford, Oxford, England OX2 0ES, United Kingdom

4. Rolls Royce plc, Allestree, Derby, England, United Kingdom

5. Rolls Royce plc, Derby, England DE24 8BJ, United Kingdom

Funder

Innovate UK

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B36663

Reference29 articles.

1. Concept and design of stators tailored to shield a fan from pressure disturbances arising in the downstream fan duct

2. Vibratory Forcing Functions Produced by Nonuniform Cascades

3. Sensitivity Analysis and Optimum Design Method for Reduced Rotor-Stator-Strut Flow Interaction

4. Interaction of fan rotor flow with downstream struts

5. Experimental investigation of unsteady fan flow interaction with downstream struts

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. A low-loss vector exhaust guide vanes and its application;Aerospace Science and Technology;2021-10

2. IMPACT OF DOWNSTREAM POTENTIAL PERTURBATIONS ON THE NONLINEAR STABILITY OF A GENERIC FAN;Journal of the Global Power and Propulsion Society;2020-12-09

3. Efficient Approach for Simulating Aperiodic Flows due to Geometry Distortions;AIAA Journal;2020-03

4. Impact of downstream potential perturbations on the nonlinear stability of a generic fan;J GLOB POWER PROPULS;2020

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