The Theoretical Research for the Rotor/Fuselage Unsteady Aerodynamic Interaction Problem

The Theoretical Research for the Rotor/Fuselage Unsteady Aerodynamic Interaction Problem

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Based on coupled unsteady panel/free-wake method, a universal analysis model was established, which provides a good prediction for the rotor/fuselage unsteady aerodynamic interaction. Considering the deficiencies of the traditional time-marching rotor free-wake algorithms, notably on stability and e...

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Bibliographic Details
Main Authors: Liu Dawei, Xin Ji, Huang Jun
Format: Article
Language:English
Published: Instituto de Aeronáutica e Espaço (IAE) 2016-08-01
Series:Journal of Aerospace Technology and Management
Subjects:
Aerodynamic interaction
Panel method
Freewake
Rotor/fuselage interaction
Online Access:https://www.jatm.com.br/jatm/article/view/686

Internet

https://www.jatm.com.br/jatm/article/view/686

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