Keyphrases
Substitute Model
100%
Cooling Air
100%
Turbofan
100%
Propulsion System
50%
Inlet Conditions
50%
Carbon Dioxide
50%
Thermodynamics
50%
Parameter Study
50%
Discretized
50%
System Level
50%
Design Parameters
50%
Water Vapor
50%
Extra Degree of Freedom
50%
Design Point
50%
Linearization
50%
Nitrogen Oxides
50%
Identified Parameters
50%
Particulate Matter
50%
Aircraft Systems
50%
Heat Exchanger
50%
Mass Flow Rate
50%
Steam Cycle
50%
Steam Injection
50%
Dual Fluid
50%
Aviation
50%
Design Drivers
50%
Climate Change Impacts
50%
System Weight
50%
Water Injection
50%
Air Mass Flow
50%
Consumption System
50%
Main Design Parameters
50%
Exchange Factor
50%
Clausius
50%
Fuel Burn
50%
Impact Reduction
50%
Joule-Brayton Cycle
50%
Air Modeling
50%
Vaporization Process
50%
Rankine
50%
Contrail Cirrus
50%
Climate Emissions
50%
Thrust Specific Fuel Consumption
50%
Engineering
Design Parameter
100%
Cooling Air
100%
Degree of Freedom
50%
Propulsion System
50%
One Dimensional
50%
Additional Degree
50%
Design Point
50%
Aircraft System
50%
Main Effect
50%
Mass Flowrate
50%
Atmospheric Aerosol
50%
Specific Fuel Consumption
50%
Air Mass Flow
50%
Vaporization
50%
Water Injection
50%
Steam Rankine Cycle
50%
Exchanger
50%
Steam Injection
50%