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西北工业大学 国内
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Rapid dynamic aeroelastic response analysis of the highly flexible wing with distributed propellers influence
X. Wu,
Z. Zhou
, Z. P. Wang
航空学院
Northwestern Polytechnical University Xian
科研成果
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探究 'Rapid dynamic aeroelastic response analysis of the highly flexible wing with distributed propellers influence' 的科研主题。它们共同构成独一无二的指纹。
分类
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Engineering
Flexible Wings
100%
Propeller
100%
Large Deformation
33%
Vortex
33%
Slipstream
33%
Computational Cost
16%
Dynamic Pressure
16%
Dynamic Response
16%
High Aspect Ratio
16%
Beam Element
16%
Response Value
16%
Rotational
16%
Lattice Method
16%
Propeller Thrust
16%
Tangential Induced Velocity
16%