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- W2376324693 abstract "The aircraft's dynamic stall aerodynamic characteristics are different from static aerodynamic characteristics after stall.In order to analyze the unsteady characteristics of airfoil,an experimental method of low-speed airfoil dynamic was presented briefly in this paper.By changing the attack angle and vibration frequency,the unsteady aerodynamic characteristics of airfoil during pitch-up movement and plunge movement were researched,and the influence of various factors was analyzed.With increase of vibration frequency,the lift will increase and stall angle will be delayed during pitch-up movement.When the frequency is small,the impact of amplitude to lift and attack angle of stall are obvious during plunge movement" @default.
- W2376324693 created "2016-06-24" @default.
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- W2376324693 date "2010-01-01" @default.
- W2376324693 modified "2023-09-23" @default.
- W2376324693 title "The Experiment Technology Investigation of Low-speed Airfoil Dynamic Aerodynamic Characters" @default.
- W2376324693 hasPublicationYear "2010" @default.
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