Engineering
Aerodynamic Performance
100%
Numerical Technique
100%
Computer Simulation
100%
Lift to Drag Ratio
50%
Angle-of-Attack
50%
Airfoil
50%
Aerodynamic Efficiency
50%
Increasing Demand
50%
Fuel Efficiency
50%
Technological Advance
50%
Flow Property
50%
Mach Number
50%
Winglets
50%
Numerical Model
50%
Operating Cost
50%
Sweep Angle
50%
Body Model
50%
Boundary Condition
50%
Air Transportation
50%
INIS
performance
100%
evaluation
100%
aircraft
100%
aerodynamics
100%
comparative evaluations
50%
design
50%
efficiency
50%
demand
50%
computerized simulation
50%
air
25%
reduction
25%
increasing
25%
optimization
25%
vehicles
25%
density
25%
simulation
25%
lifts
25%
noise
25%
drag
25%
operating cost
25%
fuels
25%
configuration
25%
boundary conditions
25%
turbulence
25%
airfoils
25%
mach number
25%