Numerical investigation of the quasi-vortex-ring state of the propulsive wing in vertical descent-Reference-Cited by-同舟云学术

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Numerical investigation of the quasi-vortex-ring state of the propulsive wing in vertical descent

Published:2023-01 Issue: Volume:132 Page:108075
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Lu Jiaxin^ORCID,Lu Yang^ORCID,Wang Junjie,Xu Xice,Shao Mengxue^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. High-lift propulsive airfoil with integrated crossflow fan;Kummer;J. Aircr.,2006

2. Simulation of the cross-flow fan and application to a propulsive airfoil concept;Kummer,2006

3. P. Mortier, Fan or blowing apparatus, U.S. Patent No. 507445, 1893.

4. Experimental investigation of embedded cross-flow fan for airfoil propulsion/circulation control;Dygert;J. Propuls. Power,2012

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1. Numerical Simulation and Experimental Study on the Aerodynamics of Propulsive Wing for a Novel Electric Vertical Take-Off and Landing Aircraft;Aerospace;2024-05-27

2. Comparison on Aerodynamic Characteristics of a Propulsive Wing and a Rotor in Hover;Proceedings of the 2024 3rd International Symposium on Intelligent Unmanned Systems and Artificial Intelligence;2024-05-17

3. Control of Aerodynamic Characteristics of Thick Airfoils at Low Reynolds Numbers Using Methods of Boundary Layer Control;Fluids;2024-01-17

4. Numerical study on the hydrodynamic performance and wake dynamics of propulsive wing propulsors with different cross-flow fans;Physics of Fluids;2024-01-01

5. A Wind Tunnel Investigation on the Aerodynamics of the Propulsion Wing for a Novel eVTOL Vehicle;SAE Technical Paper Series;2023-12-31

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