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國立陽明交通大學研發優勢分析平台 首頁
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查看斯高帕斯 (Scopus) 概要
魏世昕 Shih-Sin
助理教授
太空系統工程研究所
h-index
h10-index
h5-index
101
引文
5
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。
101
引文
5
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。
101
引文
5
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。
2016
2025
每年研究成果
概覽
指紋
網路
研究成果
(10)
類似的個人檔案
(3)
指紋
查看啟用 Shih-Sin Wei 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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Keyphrases
Author Team
11%
BarA
14%
Catalytic Bed
11%
Combustion
19%
Confined Geometry
14%
Control Vector
11%
Deep Pool
29%
Droplet Impacting
29%
F-ratio
23%
Flamelet
14%
Fuel Grain
11%
Heat-induced
11%
Hot Fire Test
15%
Hovering Flight
29%
Hybrid Rocket
35%
Hybrid Rocket Motor
59%
Hybrid Rocket Propulsion
11%
Hydrogen Peroxide
95%
Hypergolic
14%
Hypergolic Ignition
29%
Ignition
22%
Ignition Delay Time
14%
Ignition Mechanism
14%
Isopropyl Alcohol
14%
Launch Site
59%
Mass Flow Rate
20%
NaBH4
29%
National Space
11%
Numerical Investigation
29%
Oxidizer
47%
Plume
14%
Polypropylene
59%
Port Size
11%
Propulsion Performance
15%
Regenerative Cooling
29%
Regression Rate
29%
Rocket
11%
Rocket Engine
13%
Rocket Launch
23%
Rocket Propulsion Systems
29%
Seasonal Wind
11%
Sounding Rocket
29%
Swirl number
17%
Taiwan
17%
Throttleable
29%
Thrust Impulse
14%
Thrust Vector Control
17%
Weather Criteria
11%
Wind Analysis
59%
Wind Pattern
35%
Engineering
Airframe
29%
Combustion Chamber
20%
Computational Fluid Dynamics
29%
Confined Geometry
9%
Control Vector
29%
Decreasing Temperature
14%
Delay Time
9%
Design Guideline
5%
Dynamic Models
9%
Engine Design
23%
Engine Operating
14%
Engine Performance
5%
Engine System
9%
Event Camera
11%
Experimental Investigation
29%
Flamelets
23%
Flight Control
9%
Flight Test
29%
Flow Channel
5%
Hybrid Motor
29%
Hybrid Rocket Engine
53%
Ignition
35%
Ignition Delay
9%
Ignition System
11%
Insulation Material
5%
Laser Scanner
9%
Launch Site
59%
Lightweight Design
5%
Liquid Rocket Engine
9%
Manufacturing Engineering
5%
Mass Consumption
5%
Mass Flowrate
20%
Oxidizer
100%
Petri Dish
9%
Physical Phenomena
9%
Position Control
9%
Preliminary Analysis
9%
Pressure Tank
14%
Propulsion System
29%
Rate Region
9%
Real Application
14%
Rocket Engine
74%
Rocket Launch
40%
Rocket Propulsion
79%
Solid Fuel
9%
Solid Rocket Engine
9%
Specific Impulse
14%
Surface Grain
9%
Temperature Range
29%
Three Dimensional Printing
5%
