Keyphrases
Fabric Laminate
75%
Non-crimp Fabric
75%
Direct Combustion
75%
Aircraft Power
75%
Taper Ratio
75%
Steady-state Model
75%
Propulsion
75%
Aircraft Configuration
75%
Element Analysis
75%
Vapor Cloud
75%
Gasoline Vapor
75%
Vapor Diffusion
75%
Advanced Composites
75%
Residual Stress Field
75%
Technical Assessment
75%
Thermal Stress Field
75%
XR Technologies
75%
Girth Weld
75%
Line pipe
75%
Feasibility Analysis
75%
Computational Fluid Dynamics
75%
Extended Reality
75%
Bipolar Plate
75%
Proton Exchange Membrane Fuel Cell (PEMFC)
75%
Fuel Cell Performance
75%
Plate Coating
75%
Performance Characteristics
75%
Hydrogen Fuel Cell
75%
Petroleum
75%
Performance Evaluation
75%
Evaluation Model
75%
Caribbean
75%
Undergraduate Program
75%
Fuel Consumption
75%
Bare Metal
75%
Non-native
75%
Welding Materials
75%
Hopper Wagon
75%
Strut
75%
Gasoline
56%
Discrete Phase Model
56%
Wind Speed
56%
Weight Penalty
37%
Propulsion Efficiency
37%
Resistance Corrosion
37%
Combustion Cell
37%
Hydrogen Combustion
37%
Performance Capability
37%
Regional Aircraft
37%
Aircraft Type
37%
Engineering
Finite Element Method
100%
Fuel Cell
93%
Bare Metal
75%
Steady-State Model
75%
Powered Aircraft
75%
Advanced Composite
75%
Computer Aided Design
75%
Computational Fluid Dynamics
75%
Non-Crimp Fabric
75%
Virtual Reality
75%
Residual Stress
75%
Stress Field
75%
Performance Characteristic
75%
Retrofit
75%
Bipolar Plate
75%
Proton-Exchange Membrane Fuel Cells Performance
75%
Feasibility Study
75%
Thermal Stress
75%
Economic Characteristic
75%
Geometric Parameter
75%
Loading Condition
75%
Mathematical Model
75%
Phase Model
56%
Hydrogen Fuel
50%
Finite Element Modeling
43%
Coated Plate
37%
Welds
37%
Thermal History
37%
Mild Steel
37%
Austenitic Stainless Steel
37%
Thin Ply
24%
Thick Section
24%
Compressive Loading
24%
Taper Region
24%
Mass Reduction
24%
Wings
24%
Mechanical Engineering
24%
Application Area
24%
Fuel Mass
24%
Specific Fuel Consumption
24%
Direct Hydrogen Combustion
24%
Aircraft Type
24%
Potential Benefit
24%
Automotives
24%
Product Design
24%
Underpinnings
24%
Power Requirement
24%
Hydrogen Technology
24%
Composite Structure
24%
Main Factor
18%