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查看斯高帕斯 (Scopus) 概要
陳 昱達
助理教授
航空太空工程學系
電話
06-2757575 ext 63625
電子郵件
z11308024
mail.ncku.edu
tw
h-index
50
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。
2011
2025
每年研究成果
概覽
指紋
網路
研究成果
(12)
類似的個人檔案
(2)
指紋
查看啟用 Yu-Ta Chen 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。
排序方式
重量
按字母排序
Engineering
Oxidizer
100%
Autoignition
80%
Cold Flow
40%
Design Parameter
40%
Delay Time
40%
Thin Films
40%
Rocket Propulsion
40%
Ignition Delay
40%
Flow Dynamics
40%
Hydrogen Fuel
40%
Experimental Observation
40%
Resistive
40%
Fuel System
40%
Clean Air
40%
Air Blast
40%
Air Flow
40%
Atomisation
35%
Propellant System
33%
Distribution Ratio
26%
Metallizations
26%
Vortex
26%
Jet Velocity
26%
Catalytic Reaction
20%
Gas-Phase
20%
Mass Flowrate
17%
Flow Distribution
17%
Operational Condition
13%
Development Process
13%
Simplifies
13%
Optimum Design
13%
Characteristic Velocity
13%
Propellant Mass
13%
Shape Factor
13%
Axial Velocity
13%
Average Particle Size
13%
Calorific Value
10%
High Heating Value
10%
Small Gas Turbine
10%
Ignition Point
10%
Inflow Rate
10%
Heat Release
10%
Liquid Phase
10%
Ignition
10%
Conductive
6%
Room Temperature
6%
Oxygen Vacancy
6%
Nonvolatile Memory
6%
Ar Atmosphere
6%
Oxygen Ion
6%
Annealing Temperature
6%
Keyphrases
Injector Design
80%
Hypergolic
55%
Sm2Ti2O7
40%
Slinger
40%
Amorphous Nb2O5
40%
Dopant
40%
Kerosene
40%
Fuel System
40%
Dynamic Interaction
40%
Oxygen Vacancy
40%
Injector
40%
Rocket Propulsion
40%
Hydrogen Peroxide
40%
Autoignition
40%
Swirl Spray
40%
Ignition Delay Time
30%
Shock Train
30%
Multivalent
24%
Bipropellant
20%
Droplet Distribution
20%
Dual-mode Scramjet
20%
Clean Air
20%
Scram
20%
Liquid Oxidizer
18%
Propulsive Performance
18%
Contact Test
18%
Atomization Angle
17%
Band Gap
16%
Nb2O5
16%
Jet Modules
13%
Spray Interaction
13%
Uniform Set
10%
Liquid Fuel
10%
Cylindrical Chamber
10%
Hypergolic Propellant
10%
Storability
10%
Gas Phase
10%
Low Toxicity
10%
Propellant
10%
Fire Experiment
10%
Controlling Factors
10%
Liquid Phase
10%
Delay Time
10%
Impinging Injector
10%
Premixed
10%
Ignition Point
10%
Catalytic Reaction
10%
Heating Value
10%
Hot Fire Test
10%
Ignition Capability
10%
