INIS
aerodynamics
100%
performance
86%
aircraft
81%
reviews
47%
evaluation
44%
design
42%
engines
42%
air
39%
numerical analysis
32%
vehicles
31%
airfoils
30%
turbines
28%
comparative evaluations
25%
compressors
24%
failures
21%
lifts
21%
fans
21%
losses
20%
mach number
19%
transonic flow
19%
turbulence
19%
rockets
18%
rotors
17%
efficiency
17%
drag
15%
computerized simulation
15%
missiles
14%
simulation
13%
breathing
13%
surfaces
13%
applications
12%
control
12%
flow rate
12%
fuels
11%
speed
10%
combustion instability
10%
streams
10%
fins
10%
configuration
10%
velocity
10%
computer codes
9%
geometry
9%
ships
8%
safety
8%
robots
8%
flow blockage
8%
clearance
8%
casings
8%
nozzles
8%
gears
8%
Engineering
Aerodynamic Performance
48%
Numerical Technique
26%
Evaluation
26%
Development
20%
Axial-Flow Compressors
18%
Enhancement
18%
Applications
18%
Centrifugal Compressor
17%
Models
16%
Angle-of-Attack
16%
Aerodynamics
16%
Performance
15%
Mach Number
12%
Aircraft
12%
Performance Improvement
11%
Research
10%
Propeller
10%
Computational Fluid Dynamics
10%
Wings
10%
Turbulence
10%
Velocity
10%
Numerical Approach
9%
Mass Flowrate
9%
Micro Air Vehicle
8%
Mechanisms
8%
Flow Visualization
8%
Energy Harvesting
8%
Sweep Angle
8%
Carbon Fibre Composite
8%
Mechanical Design
8%
Axial Flow Fan
8%
Robot
8%
Jet Engine
8%
Transonic Flow
8%
Ship Propellers
8%
Surfaces
8%
Commercial Vehicle
8%
Response Surface Method
8%
Diesel Engine
8%
Oil
8%
Composite Pressure Vessel
8%
Re-Entry Vehicle
8%
Material Component
8%
Fluid Flow
8%
Horizontal Axis Wind Turbine
8%
Alternative Fuel
8%
Airfoil
8%
Control Flow
8%
Compressor Stage
8%
Temperature
7%
Physics
Aerodynamics
37%
Performance
28%
Axial Flow Turbines
17%
Simulation
12%
Mach Number
11%
Aerodynamic Characteristic
11%
Combustion Stability
10%
Angle of Attack
10%
Model
10%
Missiles
10%
Evaluation
8%
Failure Analysis
8%
Research Aircraft
8%
Energy Harvesting
8%
Axial Flow
8%
Air
8%
Turbulence
8%
Engine
8%
Projectile
8%
Reentry Vehicle
8%
Electromagnetics
8%
Flow Control
8%
Pressure
8%
Computational Fluid Dynamics
6%
Space Shuttle
5%
Failure
5%
