Non-axisymmetric design and flow field analysis of boundary layer ingesting fans-Reference-Cited by-同舟云学术

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Non-axisymmetric design and flow field analysis of boundary layer ingesting fans

Published:2023-09 Issue: Volume:140 Page:108429
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Yu Junyang^ORCID,Fu Wenguang,Wang Weijia,Sun Peng^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference44 articles.

1. Review of Propulsion Technologies for N+3 Subsonic Vehicle Concepts;Ashcraft,2011

2. Review of evolving trends in blended wing body aircraft design;Okonkwo;Prog. Aerosp. Sci.,2016

3. Numerical simulation for the differences between FTN/WPN engine models aerodynamic influence on BWB300 airframe;Yu;Eng. Appl. Comput. Fluid Mech.,2020

4. Performance of a boundary layer ingesting (BLI) propulsion system;Plas,2007

5. Analysis of fan stage conceptual design attributes for boundary layer ingestion;Hall;J. Turbomach.,2017

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. Design and aerodynamic stability improvement study of a non-axisymmetric stator fan in a distorted insertion plate configuration;Aerospace Science and Technology;2024-12

2. Effects of labyrinth seal with jet structure on the performance of a compressor cascade;Physics of Fluids;2024-08-01

3. Behavior of flow distortion within a boundary layer ingestion inlet;Aerospace Science and Technology;2024-03

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