Keyphrases
All Flow Regimes
22%
Axial Compressor
17%
Blade Design
29%
Blade Geometry
29%
Blade Rows
15%
Blade Shape
15%
Blade Surface
16%
Blade Thickness
11%
Body Force
15%
Boundary Layer Control
15%
Choke Margin
11%
Circulation Control
15%
Circulation Method
22%
Compressor Blade
26%
Computational Fluid Dynamics
12%
Cross Flow Fan
15%
Design Calculation
24%
Design Improvement
24%
Finite Thickness
15%
Flow Quantity
11%
Flow Restriction
11%
Flow-through
18%
Forcing Term
15%
Hypersonic
22%
Impulse Turbine
11%
Inlet Guide Vane
11%
Inverse Method
69%
Inverse Mode
16%
Inviscid Flow
15%
Loading Distribution
15%
Manufacturing Feature
11%
Modified Blades
11%
Operating Point
11%
Pressure Loading
27%
Process Compressor
11%
Propulsion
15%
Rotor 67
15%
Steady Blowing
15%
Syracuse University
15%
Tangency Condition
11%
Thickness Distribution
13%
Thin-walled Blade
11%
Three-dimensional (3D)
24%
Through-flow Method
22%
Time Marching
16%
Transonic Flow
18%
Turbine Blade
11%
Turbomachine
22%
Turbomachine Blades
40%
University Centers
15%
Engineering
Air Quality
8%
Airfoil
11%
Axial Compressors
25%
Blade Geometry
39%
Blade Row
18%
Blade Surface
32%
Blade Thickness
10%
Blades Design
35%
Body Force
11%
Boundary Condition
13%
Breathing Zone
8%
Cabins (Aircraft)
7%
Circulation Control
15%
Compressor Blades
34%
Computational Fluid Dynamics
14%
Design Calculation
24%
Design Method
24%
Diffusion Coefficient
7%
Electric Inductors
11%
Euler Equation
22%
Exhaust Temperature
7%
Experimental Investigation
7%
Flow Quantity
8%
Flow Regime
25%
Guide Vane
11%
Heating Power
7%
Impulse Turbine
11%
Inverse Design
15%
Inverse Design Method
10%
Inverse Method
100%
Inverse Mode
13%
Inviscid Flow
22%
Mannequin
7%
Momentum Flux
7%
Momentum Thickness
9%
Natural Ventilation
9%
Numerical Solution
7%
Operating Point
10%
Rise Building
7%
Rotors
34%
Stepping Scheme
12%
Supersonic Flow
11%
Thermal Manikin
10%
Thickness Distribution
18%
Throughflow
22%
Transonic Flow
26%
Turbomachine Blades
48%
Turbomachinery
11%
Turbomachines
30%
Two Dimensional
11%