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查看斯高帕斯 (Scopus) 概要
賴 錦文
教授
機械工程學系
https://orcid.org/0000-0002-1380-8282
電話
03-5712121#55123
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engp4324
nycu.edu
tw
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https://aerotech.lab.nycu.edu.tw/index.php/en/about-us/
h-index
h10-index
h5-index
1130
引文
20
h-指數
按照存儲在普爾（Pure）的出版物數量及斯高帕斯（Scopus）引文計算。
698
引文
16
h-指數
按照存儲在普爾（Pure）的出版物數量及斯高帕斯（Scopus）引文計算。
146
引文
7
h-指數
按照存儲在普爾（Pure）的出版物數量及斯高帕斯（Scopus）引文計算。
1998 …
2024
每年研究成果
概覽
指紋
網路
計畫
(9)
研究成果
(68)
類似的個人檔案
(6)
指紋
查看啟用 Kim Boon Lua 的研究主題。這些主題標籤來自此人的作品。共同形成了獨特的指紋。
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重量
按字母排序
Keyphrases
Two Dimensional
95%
Flapping Wing
58%
Hovering
47%
Reynolds number
38%
Leading Edge Vortex
38%
Ogive
36%
Side Force
36%
Flap
32%
Aerodynamic Force
32%
Aerodynamics
31%
Vortex
29%
Elliptic Airfoil
28%
Three-dimensional (3D)
25%
Wing-wake Interaction
24%
Force Generation
24%
Forward Flight
23%
Thrust Performance
22%
Vortex-induced Vibration
21%
Taylor-Couette Flow
21%
Flow Structure
20%
Airfoil
20%
Phase Angle
19%
Flapping Frequency
19%
Flow Field
18%
Flapping Motion
18%
Angle of Attack
16%
In Tandem
16%
Edge Pattern
15%
Streamwise Counter-rotating Vortices
15%
Flat Plate Boundary Layer
15%
Rear Wing
15%
Flapping-wing Micro Aerial Vehicles (FWMAVs)
15%
Wind Energy Harvesting
15%
Corrugated Surface
15%
Wake Structure
15%
Lift Generation
15%
Axial Flow
15%
Front Wing
14%
Numerical Investigation
13%
Digital Particle Image Velocimetry
12%
Circular Cylinder
12%
Cross-flow
12%
Force Sensor
11%
Tandem Configuration
11%
Heave
11%
Wake Capture
11%
Lift Coefficient
10%
Effective Angle of Attack
10%
Non-axisymmetric
10%
Tandem Flapping Wings
10%
Engineering
Two Dimensional
100%
Vortex
73%
Airfoil
47%
Reynolds' Number
40%
Leading Edge Vortex
40%
Aerodynamic Force
36%
Angle-of-Attack
34%
Numerical Study
34%
Sideforce
31%
Force Generation
31%
Flow Structure
26%
Leading Edge
25%
Lift Coefficient
25%
Forward Flight
24%
Phase Shift
23%
Particle Image Velocimetry
22%
Couette Flow
21%
Vortex Induced Vibration
21%
Rotating Vortex
18%
Computer Simulation
17%
Drag Coefficient
17%
Axisymmetric
17%
Streamwise
17%
Circular Cylinder
16%
Micro Air Vehicle
16%
Flat Plate Boundary Layer
15%
Front Wing
15%
Microelectromechanical System
15%
Energy Harvesting
15%
Wind Power
15%
Flow Distribution
15%
Vortex Shedding
13%
Effective Angle of Attack
12%
Axial Flow
11%
Aspect Ratio
11%
Transients
11%
Aerodynamic Effect
10%
Ground Effect
10%
Piezoelectric
10%
Piezoresistor
10%
Drag Reduction
10%
Harvester
10%
Trailing Edge
10%
Energy Engineering
9%
Pressure Distribution
9%
Harmonics
9%
Rotation Rate
9%
Rotational Motion
8%
Secondary Flow
8%
Fluid Mechanics
8%
