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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
122
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。
122
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。
122
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
2026
每年研究成果
概覽
指紋
網路
研究成果
(13)
類似的個人檔案
(2)
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
Ambient Temperature
29%
Average Thrust
29%
BarA
16%
Catalyst Bed
29%
Combustion
24%
Diethylenetriamine
29%
Engine Design
29%
Ethylenediamine
29%
Fuel Grain
33%
Gasses
17%
High-speed Flight
19%
High-test Peroxide
22%
Hot Fire Test
44%
Hybrid Rocket
58%
Hybrid Rocket Motor
100%
Hybrid Rocket Propulsion
88%
Hydrogen Peroxide
58%
Hypergolic
53%
Hypergolic Propellant
50%
Ignition Delay Time
40%
Ignition Mechanism
14%
Indigenous Spaces
29%
Launch Site
39%
Lessons Learned
29%
NaBH4
35%
New Space
19%
Nitrous Oxide
29%
Numerical Investigation
29%
Oxidizer
49%
Paraffin
29%
Performance Investigation
29%
Performance Stability
29%
Polypropylene
68%
Potassium Nitrate
29%
Regenerative Cooling
29%
Regression Rate
29%
Rocket
16%
Rocket Launch
21%
Rocket Propulsion Systems
29%
Solid Propellant
29%
Sounding Rocket
61%
Space Development
29%
Specific Impulse
16%
Swirl number
17%
Temperature Range
29%
Thrust Impulse
14%
Total Impulse
49%
Transonic Aerodynamics
29%
Wind Analysis
29%
Wind Pattern
17%
Engineering
Aerodynamics
29%
Airframe
29%
Catalyst Bed
29%
Chamber Pressure
7%
Combustion Chamber
19%
Computational Fluid Dynamics
29%
Confined Geometry
11%
Decreasing Temperature
14%
Delay Time
41%
Dynamic Models
9%
Engine Design
23%
Engine Operating
14%
Engine Performance
5%
Engineering
44%
Event Camera
5%
Experimental Investigation
29%
Experimental Platform
29%
Flamelets
11%
Flight Data
29%
Flight Test
18%
Hybrid Motor
29%
Hybrid Rocket Engine
57%
Hydrogen
40%
Ignition
41%
Ignition Delay
41%
Ignition System
5%
Insulation Material
5%
Laser Scanner
9%
Launch Site
58%
Manufacturing Engineering
5%
Mass Flowrate
21%
Oxidizer
88%
Petri Dish
11%
Physical Phenomena
9%
Pressure Tank
14%
Propulsion System
29%
Rate Region
9%
Real Application
14%
Rocket Engine
64%
Rocket Launch
49%
Rocket Propulsion
88%
Scaling Law
6%
Solid Fuel
14%
Specific Impulse
16%
Structural Design
29%
Surface Grain
9%
Technical Challenge
14%
Temperature Range
29%
Test Result
7%
Three Dimensional Printing
5%
