Numerical study on the Re effects on the tip flow structures of transonic fan under inlet distortion-Reference-Cited by-同舟云学术

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Numerical study on the Re effects on the tip flow structures of transonic fan under inlet distortion

Published:2023-10 Issue: Volume:141 Page:108530
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Li Zhiping,Zhu Xingyu^ORCID,Yan Zhaoqi,Pan Tianyu^ORCID,Zheng Xinqian

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference42 articles.

1. Wake ingestion propulsion benefit;Smith;J. Propuls. Power,1993

2. Engine conceptual design studies for a hybrid wing body aircraft;Tong,2009

3. Parametric design studies for propulsive fuselage aircraft concepts;Seitz;CAES Aeronaut. J.,2015

4. Installation effects of a propeller mounted on a high-lift wing with a Coanda flap. Part I: aeroacoustic experiments;Akkermans,2014

5. Installation effects of a propeller mounted on a wing with Coanda flap. Part II: numerical investigation and experimental validation experiments;Dierke,2014

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