Engineering
Aerodynamic Interference
45%
Aerodynamic Model
40%
Aerodynamic Performance
5%
Airframe
16%
Blade Model
16%
Blade Span
11%
Combined Method
16%
Computational Fluid Dynamics
16%
Computational Time
11%
Computer Simulation
33%
Conventional Propeller
45%
Discretization
11%
Execution Time
6%
Failure Event
5%
Free Vortex
74%
Genetic Algorithm
13%
Induced Velocity
33%
Lifting Line
16%
Loading Condition
16%
Main Conclusion
5%
Marginals
33%
Objective Function
6%
Operating Point
6%
Optimisation Problem
6%
Particle Swarm Optimization
13%
Performance Parameter
11%
Potential Failure
5%
Power Budget
33%
Power Ratio
18%
Power Requirement
5%
Propeller
67%
Propeller Geometry
33%
Propeller Thrust
16%
Propulsion System
9%
Propulsive Efficiency
33%
Rotor Position
6%
Rotor System
45%
Rotorcraft
50%
Rotors
100%
Scale Variation
16%
Separation Distance
11%
Size Parameter
11%
Static Thrust
33%
System Component
5%
Systems Performance
11%
Takeoff Weight
7%
Thrust Power
33%
Two Dimensional
6%
Velocity Field
11%
Vortex
33%
