Research on Numerical Calculation for Aerodynamic Characteristics Analysis of Ducted Fan

By taking a typical ducted fan system model as the research object, the unsteady aerodynamics calculation method is established based on slide dynamic mesh technology. After the experimental validation of calculation method, the influence factors of viscous effect, tip clearance and propeller disk l...

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Format: Article
Language:zho
Published: EDP Sciences 2018-12-01
Series:Xibei Gongye Daxue Xuebao
Subjects:
Online Access:https://www.jnwpu.org/articles/jnwpu/pdf/2018/06/jnwpu2018366p1045.pdf
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collection DOAJ
description By taking a typical ducted fan system model as the research object, the unsteady aerodynamics calculation method is established based on slide dynamic mesh technology. After the experimental validation of calculation method, the influence factors of viscous effect, tip clearance and propeller disk location are analyzed based on numerical calculation. The research results show that, the viscous effect embodies the boundary layer interactions between propeller tip and duct, and the calculation accuracy can be improved by considering viscous effect; the tip clearance determines the influence effect of propeller, and the decreasing of tip clearance leads to the increasing of duct thrust; the propeller disk location determines the flow quality and tip clearance, a reasonable location must bring the optimal fairing effect and ensures the tip clearance meeting the design requirements.
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spelling doaj.art-f7cba8a52bbb44b2bb19541bba11d11a2023-11-02T01:12:46ZzhoEDP SciencesXibei Gongye Daxue Xuebao1000-27582609-71252018-12-013661045105110.1051/jnwpu/20183661045jnwpu2018366p1045Research on Numerical Calculation for Aerodynamic Characteristics Analysis of Ducted Fan012School of Aeronautics, Northwestern Polytechnical UniversitySchool of Astronautics and Aeronautics, Tsinghua UniversityChinese Aeronautical Ratio and Electronics Research InstituteBy taking a typical ducted fan system model as the research object, the unsteady aerodynamics calculation method is established based on slide dynamic mesh technology. After the experimental validation of calculation method, the influence factors of viscous effect, tip clearance and propeller disk location are analyzed based on numerical calculation. The research results show that, the viscous effect embodies the boundary layer interactions between propeller tip and duct, and the calculation accuracy can be improved by considering viscous effect; the tip clearance determines the influence effect of propeller, and the decreasing of tip clearance leads to the increasing of duct thrust; the propeller disk location determines the flow quality and tip clearance, a reasonable location must bring the optimal fairing effect and ensures the tip clearance meeting the design requirements.https://www.jnwpu.org/articles/jnwpu/pdf/2018/06/jnwpu2018366p1045.pdfducted fanviscous effecttip clearancepropeller disk locationdynamic meshunsteady aerodynamics
spellingShingle Research on Numerical Calculation for Aerodynamic Characteristics Analysis of Ducted Fan
Xibei Gongye Daxue Xuebao
ducted fan
viscous effect
tip clearance
propeller disk location
dynamic mesh
unsteady aerodynamics
title Research on Numerical Calculation for Aerodynamic Characteristics Analysis of Ducted Fan
title_full Research on Numerical Calculation for Aerodynamic Characteristics Analysis of Ducted Fan
title_fullStr Research on Numerical Calculation for Aerodynamic Characteristics Analysis of Ducted Fan
title_full_unstemmed Research on Numerical Calculation for Aerodynamic Characteristics Analysis of Ducted Fan
title_short Research on Numerical Calculation for Aerodynamic Characteristics Analysis of Ducted Fan
title_sort research on numerical calculation for aerodynamic characteristics analysis of ducted fan
topic ducted fan
viscous effect
tip clearance
propeller disk location
dynamic mesh
unsteady aerodynamics
url https://www.jnwpu.org/articles/jnwpu/pdf/2018/06/jnwpu2018366p1045.pdf