Keyphrases
Direct Combustion
88%
Fuel Consumption
74%
Propulsion
59%
Performance Characteristics
59%
Fuel Cell
55%
Fabric Laminate
44%
Non-crimp Fabric
44%
Aircraft Power
44%
Taper Ratio
44%
Steady-state Model
44%
Aircraft Configuration
44%
Element Analysis
44%
Vapor Cloud
44%
Gasoline Vapor
44%
Vapor Diffusion
44%
Advanced Composites
44%
Residual Stress Field
44%
Technical Assessment
44%
Thermal Stress Field
44%
XR Technologies
44%
Girth Weld
44%
Line pipe
44%
Feasibility Analysis
44%
Computational Fluid Dynamics
44%
Extended Reality
44%
Bipolar Plate
44%
Proton Exchange Membrane Fuel Cell (PEMFC)
44%
Fuel Cell Performance
44%
Plate Coating
44%
Hydrogen Fuel Cell
44%
Petroleum
44%
Performance Evaluation
44%
Evaluation Model
44%
Caribbean
44%
Undergraduate Program
44%
Bare Metal
44%
Non-native
44%
Welding Materials
44%
Hopper Wagon
44%
Strut
44%
Technology Readiness
44%
Late Development
44%
Aviation
44%
Hydrogen Technologies
37%
Gasoline
33%
Discrete Phase Model
33%
Wind Speed
33%
Power Requirement
22%
Weight Penalty
22%
Propulsion Efficiency
22%
Engineering
Fuel Cell
100%
Computational Fluid Dynamics
88%
Retrofit
88%
Finite Element Analysis
59%
Powered Aircraft
59%
Performance Characteristic
59%
Steady-State Model
44%
Advanced Composite
44%
Non-Crimp Fabric
44%
Virtual Reality
44%
Residual Stress
44%
Stress Field
44%
Feasibility Study
44%
Thermal Stress
44%
Economic Characteristic
44%
Geometric Parameter
44%
Loading Condition
44%
Mathematical Model
44%
Computer Aided Design
44%
Bipolar Plate
44%
Bare Metal
44%
Proton-Exchange Membrane Fuel Cells Performance
44%
Aerodynamic Characteristic
44%
Phase Model
33%
Hydrogen Fuel
29%
Flaps
29%
Drag Reduction
29%
Lift Coefficient
29%
Experimental Measurement
29%
Hydrogen Technology
29%
Finite Element Modeling
25%
Thermal History
22%
Mild Steel
22%
Austenitic Stainless Steel
22%
Welds
22%
Coated Plate
22%
Angle-of-Attack
14%
Thin Ply
14%
Thick Section
14%
Compressive Loading
14%
Taper Region
14%
Mass Reduction
14%
Wings
14%
Mechanical Engineering
14%
Application Area
14%
Fuel Mass
14%
Specific Fuel Consumption
14%
Direct Hydrogen Combustion
14%
Aircraft Type
14%
Potential Benefit
14%