A REVIEW OF NUMERICAL RESEARCH ON AEROELASTIC DYNAMICAL RESPONSE OF AERO-ENGINE BLADES

ZHANG Zhang; HOU Anping; TUO Wei; XIA Aiguo

doi:10.6052/1000-0992-11-121

Volume 42 Issue 5

Sep. 2012

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ZHANG Zhang, HOU Anping, TUO Wei, XIA Aiguo. A REVIEW OF NUMERICAL RESEARCH ON AEROELASTIC DYNAMICAL RESPONSE OF AERO-ENGINE BLADES[J]. Advances in Mechanics, 2012, 42(5): 572-582. doi: 10.6052/1000-0992-11-121

Citation:

ZHANG Zhang, HOU Anping, TUO Wei, XIA Aiguo. A REVIEW OF NUMERICAL RESEARCH ON AEROELASTIC DYNAMICAL RESPONSE OF AERO-ENGINE BLADES[J]. Advances in Mechanics, 2012, 42(5): 572-582. doi: 10.6052/1000-0992-11-121

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A REVIEW OF NUMERICAL RESEARCH ON AEROELASTIC DYNAMICAL RESPONSE OF AERO-ENGINE BLADES

doi: 10.6052/1000-0992-11-121

1.
Chinese National Key Laboratory of Aerodynamics & Thermodynamics on Aero-engine, Beihang University, Beijing 100191, China
2. Beijing Aeronautical Technology Research Center, Beijing 100076, China

Funds: The project was supported by the National Natural Science Foundation of China (60934001).

More Information

Corresponding author: ZHANG Zhang
Received Date: 2011-08-29
Rev Recd Date: 2012-05-25
Publish Date: 2012-09-25

Abstract

Abstract

The high cycle fatigue failure of aero-engine blades occurs frequently.Aeroelastic dynamic response is a major concern in engineer applications.A review of numerical researches on blade aeroelastic dynamic response is presented in the paper,including numerical simulation,test study and possible research trends.The flow-induced vibration mechanism of blade dynamic response and the numerical method about fluid-structure interaction will be the focus in further mechanism study.For engineer applications,it is valuable to develop a prediction model for dynamic response and to evaluate its potential risks with resonance in the design process.And more attention should be paid on the aerodynamic damping technology based on flow control.
- blade,
- aeroelasticity,
- dynamic response,
- numerical simulation,
- fluid-structure interaction

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References(84)

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