Behavior of flow distortion within a boundary layer ingestion inlet-Reference-Cited by-同舟云学术

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Behavior of flow distortion within a boundary layer ingestion inlet

Published:2024-03 Issue: Volume:146 Page:108947
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Kun,Liu Lei,Huang He-xia,Tan Hui-jun,Tang Xue-bin,Zheng Gao-jie

Funder

National Natural Science Foundation of China

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Reference42 articles.

1. Power balance in aerodynamic flows;Drela;AIAA J,2009

2. Boundary layer ingestion propulsion benefit for Transport Aircraft;Hall;J. Propuls. Power,2017

3. Artificial thickening of a transonic boundary layer for the NASA tail cone thruster boundary layer ingestion concept;Jones;AIAA 2020 SciTech Forum,2020

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

5. The jet airplane utilizing boundary layer air for propulsion;Smith;J. Aeron. Sci.,1947

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. Experimental investigation of the aerodynamics of a UAV inlet with double 90° bends;Aerospace Science and Technology;2024-11

2. Experimental Study of the Aerodynamic Performance and Flow Characteristics of an Integrated UAV Inlet with Double 90° Bends;Aerospace;2024-07-21

3. Stability Enhancement of an Axial Fan by Foam Metal Casing Treatment Subjected to Circumferential Inlet Distortion;2024

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