INIS
design
100%
hybrids
100%
interactions
100%
synthesis
100%
aircraft
100%
propulsion
100%
range
80%
values
60%
power
40%
propulsion systems
40%
energy efficiency
40%
boundary layers
20%
levels
20%
coverings
20%
distribution
20%
universities
20%
mach number
20%
ingestion
20%
yields
20%
performance
20%
configuration
20%
loading
20%
Engineering
Aircraft
100%
Hybrid
100%
Design
100%
Shaft Power
40%
Power Ratio
40%
Propulsion System
40%
Energy Conservation
40%
Energy Efficiency
40%
Takeoff
40%
Electric Propulsion
40%
Blade Tip
20%
Mach Number
20%
Performance
20%
Level Requirement
20%
Local Optimum
20%
Low Value
20%
Wings
20%
Boundary Layer
20%
Applied Technology
20%
Leading Edge
20%
Propeller Blade
20%
Keyphrases
Blade Loading Distribution
25%
Wing Leading Edge
25%