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A Numerical Study on the Influence of the Rear Wing Size on the Thrust Performance of the Two Dimensional Tandem Flapping Wings
S. Nishanth, Sunil Manohar Dash,
Kim Boon Lua
機械工程學系
研究成果
:
Conference contribution
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同行評審
3
引文 斯高帕斯(Scopus)
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Keyphrases
Aspect Ratio
20%
Chord Length
80%
Constructive Interaction
20%
Flap
20%
Flapping Mode
60%
Flow Regime
40%
Flow Transients
20%
Flow Vortex
20%
Front Wing
100%
High Thrust
20%
In Tandem
20%
Leading Edge Vortex
20%
Phase Angle
20%
Rear Wing
100%
Reynolds number
20%
Shear Layer
20%
Starting Phase
20%
Strouhal number
20%
Tandem Flapping Wings
100%
Thrust Coefficient
20%
Thrust Force
20%
Thrust Performance
100%
Two Dimensional
100%
Vortex Structure
20%
Wing Length
100%
Engineering
Aspect Ratio
20%
Chord Length
80%
Flow Regime
40%
Front Wing
100%
High Thrust
20%
Leading Edge Vortex
20%
Numerical Study
100%
Phase Shift
20%
Reynolds' Number
20%
Shear Layer
20%
Strouhal Number
20%
Thrust Force
20%
Transients
40%
Two Dimensional
100%
Vortex
20%