INIS
hybrids
100%
transport
100%
aerodynamics
100%
performance
100%
aircraft
100%
propulsion
100%
reduction
66%
propulsion systems
50%
efficiency
50%
levels
33%
weight
33%
lifts
33%
drag
33%
energy consumption
33%
metrics
16%
fuels
16%
coupling
16%
geometry
16%
losses
16%
comparative evaluations
16%
passengers
16%
experimental data
16%
modeling
16%
sizing
16%
Engineering
Transport Aircraft
100%
Aerodynamic Performance
100%
Wings
100%
Aircraft
66%
Reduction
66%
Propulsion System
50%
Numerical Methods
33%
Energy Engineering
33%
Couplings
16%
Aerodynamic Modeling
16%
Aircraft Level
16%
Drivetrain
16%
Metrics
16%
Enhancement
16%
Determines
16%
Takeoff
16%
Cruise Condition
16%
Experiments
16%
Component Level
16%
Powertrain Weight
16%
Lift to Drag Ratio
16%
Aerodynamics
16%