Blowing–Suction Control in S-Shaped Inlet and Its Impact on Fan-Stage Performance-Reference-Cited by-同舟云学术

Blowing–Suction Control in S-Shaped Inlet and Its Impact on Fan-Stage Performance

Published:2019-09 Issue:9 Volume:57 Page:3954-3968
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Lei Liu¹,Fu Chen²,Kun Luo³,Huachen Pan¹,Huawei Qin¹,Fang Wang¹,Maoying Zhou¹,Xiaoqing Tian¹

Affiliation:

1. Hangzhou Dianzi University, 310018 Hangzhou, People’s Republic of China

2. Harbin Institute of Technology, 150001 Harbin, People’s Republic of China

3. Zhejiang University, 310027 Hangzhou, People’s Republic of China

Funder

the Public Welfare Technology Foundation of Zhejiang Province in China

the Open Project of State Key Laboratory of Clean Energy Utilization, Zhejiang University

the Foundation of Key Research and Development Plan in Zhejiang Province in China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference18 articles.

1. BerrierB. L.CarterM. B.AllanB. G. “High Reynolds Number Investigation of a Flush-Mounted, S-Duct Inlet with Large Amounts of Boundary Layer Ingestion,” Langley Research Center NASA TP-2005-213766 N, Hampton, VA, 2005.

2. Flow Control by Pulsed Jet in a Curved S-Duct: A Spectral Analysis

3. Experimental and numerical investigation on steady blowing flow control within a compact inlet duct

4. Active Flow Control of a Boundary Layer-Ingesting Serpentine Inlet Diffuser

5. Effectiveness of vortex generator jets and wall suction on separated flows in serpentine-duct diffuser

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