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Proceedings Papers
Volume 2A: Turbomachinery
Axial Flow Fan and Compressor Aerodynamics
The Effect of an Eroded Leading Edge on the Aerodynamic Performance of a Transonic Fan Blade Cascade
GT 2014; V02AT37A001https://doi.org/10.1115/GT2014-25023
Topics:
Blades
,
Cascades (Fluid dynamics)
,
Shock (Mechanics)
,
Shapes
,
Chords (Trusses)
,
Erosion
,
Inflow
,
Suction
,
Boundary layers
,
Bubbles
Ejector Tip Injection for Active Compressor Stabilization
GT 2014; V02AT37A004https://doi.org/10.1115/GT2014-25073
Topics:
Compressors
,
Ejectors
,
Engines
,
Flow (Dynamics)
,
Propulsion
,
Pumps
,
Design
,
Pressure
,
Stability
,
Algorithms
Riblet Application in Compressors: Towards Efficient Blade Design?
GT 2014; V02AT37A006https://doi.org/10.1115/GT2014-25142
Topics:
Blades
,
Compressors
,
Design
,
Cascades (Fluid dynamics)
,
Reynolds number
,
Manufacturing
,
Optimization
,
Suction
,
Turbulence
,
Coating processes
Endwall Contouring and Fillet Design for Reducing Losses and Homogenizing the Outflow of a Compressor Cascade
GT 2014; V02AT37A007https://doi.org/10.1115/GT2014-25277
Topics:
Cascades (Fluid dynamics)
,
Compressors
,
Design
,
Outflow
,
Pressure
,
Inflow
,
Blades
,
Corners (Structural elements)
,
Flow (Dynamics)
,
Mach number
Experimental Investigation of Tip Clearance Flow in a Transonic Compressor With and Without Plasma Actuators
GT 2014; V02AT37A008https://doi.org/10.1115/GT2014-25294
Topics:
Actuators
,
Clearances (Engineering)
,
Compressors
,
Flow (Dynamics)
,
Plasmas (Ionized gases)
,
Flow control
,
Design
,
Pressure
,
Blades
,
Rotors
Numerical Investigation on the Effect of Vortex Generator on Axial Compressor Performance
GT 2014; V02AT37A010https://doi.org/10.1115/GT2014-25329
Topics:
Compressors
,
Generators
,
Vortices
,
Blades
,
Flow (Dynamics)
,
Computational fluid dynamics
,
Cross-flow
,
Rotors
,
Boundary layers
,
Chords (Trusses)
Numerical Investigation on the Effects of Circumferential Coverage of Injection in a Transonic Compressor With Discrete Tip Injection
GT 2014; V02AT37A012https://doi.org/10.1115/GT2014-25420
Topics:
Compressors
,
Stability
,
Ejectors
,
Pressure
,
Blades
,
Computer simulation
,
Flow (Dynamics)
,
Rotors
,
Unsteady flow
Numerical Investigation of the Solidity Effect on Linear Compressor Cascades
GT 2014; V02AT37A013https://doi.org/10.1115/GT2014-25532
Topics:
Compressors
,
Blades
,
Cascades (Fluid dynamics)
,
Design
,
Chords (Trusses)
,
Mach number
,
Stability
,
Compressible flow
,
Computer software
,
Diffusion (Physics)
Numerical Investigation of Axial Compressor Stages With Differing Degrees of Reaction
GT 2014; V02AT37A015https://doi.org/10.1115/GT2014-25642
Topics:
Compressors
,
Flow (Dynamics)
,
Pressure
,
Rotors
,
Stators
,
Airfoils
,
Clearances (Engineering)
,
High pressure (Physics)
,
Leakage flows
,
Stall behavior
Experimental Investigation on Droplet Behaviour in a Transonic Compressor Cascade
GT 2014; V02AT37A016https://doi.org/10.1115/GT2014-25645
Topics:
Cascades (Fluid dynamics)
,
Compressors
,
Drops
,
Flow (Dynamics)
,
Water
,
Blades
,
Industrial gases
,
Sprays
,
Stress
,
Thin films
Combination of Active and Passive Flow Control in a High Speed Compressor Cascade
GT 2014; V02AT37A017https://doi.org/10.1115/GT2014-25662
Topics:
Cascades (Fluid dynamics)
,
Compressors
,
Flow control
,
Suction
,
Boundary layers
,
Flow (Dynamics)
,
Mach number
,
Chords (Trusses)
,
Flow visualization
,
Inflow
Experimental Study of Effects of Bowed Blade on the Flow Field in a Cantilevered Stator Passage
GT 2014; V02AT37A018https://doi.org/10.1115/GT2014-25766
Topics:
Blades
,
Flow (Dynamics)
,
Stators
,
Vortices
,
Compressors
,
Leakage
,
Clearances (Engineering)
,
Pressure
,
Probes
,
Separation (Technology)
Numerical Investigation of the Aerodynamic Behaviour of a Compressor Bleed-Air System
GT 2014; V02AT37A021https://doi.org/10.1115/GT2014-25822
Topics:
Compressors
,
Flow (Dynamics)
,
Pressure
,
Design
,
Blades
,
Cooling
,
Corners (Structural elements)
,
Engine design
,
Engineering simulation
,
Engines
A Novel Transonic Fan Swept Outlet Guide Vane Using 3D Design Optimization
GT 2014; V02AT37A022https://doi.org/10.1115/GT2014-25857
Topics:
Design
,
Guide vanes
,
Optimization
,
Blades
,
Geometry
,
Chords (Trusses)
,
Flow (Dynamics)
,
Engines
,
Physics
,
Pressure gradient
Effect of the Stator Hub Configuration and Stage Design Parameters on Aerodynamic Loss in Axial Compressors
GT 2014; V02AT37A025https://doi.org/10.1115/GT2014-26095
Topics:
Compressors
,
Design
,
Stators
,
Flow (Dynamics)
,
Leakage
,
Leakage flows
,
Clearances (Engineering)
,
Computational fluid dynamics
,
Pressure
,
Chords (Trusses)
Performance Characterization of the Effect of Axial Positioning of Bend Skewed Casing Treatment Retrofitted to a Transonic Axial Flow Compressor
Dilipkumar B. Alone, Subramani Satish Kumar, Shobhavathy Thimmaiah, Janaki Rami Reddy Mudipalli, A. M. Pradeep, Srinivasan Ramamurthy, Venkat S. Iyengar
GT 2014; V02AT37A026https://doi.org/10.1115/GT2014-26099
Topics:
Axial flow
,
Performance characterization
,
Compressors
,
Rotors
,
Chords (Trusses)
,
Aircraft engines
,
Blades
,
Design
,
Flow (Dynamics)
,
Geometry
Experimental Investigation on the Effect of Porosity of Bend Skewed Casing Treatment on a Single Stage Transonic Axial Flow Compressor
Dilipkumar B. Alone, Subramani Satish Kumar, Shobhavathy Thimmaiah, Janaki Rami Reddy Mudipalli, A. M. Pradeep, Srinivasan Ramamurthy, Venkat S. Iyengar
GT 2014; V02AT37A027https://doi.org/10.1115/GT2014-26102
Topics:
Axial flow
,
Porosity
,
Compressors
,
Flow (Dynamics)
,
Rotors
,
Blades
,
Chords (Trusses)
,
Design
,
Mach number
,
Pressure
On Understanding the Effect of Plenum Chamber of a Bend Skewed Casing Treatment on the Performance of a Transonic Axial Flow Compressor
Dilipkumar B. Alone, Subramani Satish Kumar, Shobhavathy Thimmaiah, Janaki Rami Reddy Mudipalli, A. M. Pradeep, Srinivasan Ramamurthy, Venkat S. Iyengar
GT 2014; V02AT37A028https://doi.org/10.1115/GT2014-26103
Topics:
Axial flow
,
Compressors
,
Porosity
,
Rotors
,
Blades
,
Chords (Trusses)
,
Design
,
Flow (Dynamics)
,
Geometry
,
Rotation
An Experimental Investigation of a Tandem Stator Flow Characteristic in a Low Speed Axial Research Compressor
GT 2014; V02AT37A029https://doi.org/10.1115/GT2014-26104
Topics:
Compressors
,
Flow (Dynamics)
,
Stators
,
Design
,
Blades
,
Fluids
,
Guide vanes
,
High pressure (Physics)
,
Jet engines
,
Power density
Effects of the Steady Wake-Tip Clearance Vortex Interaction in a Compressor Cascade: Part I — Experimental Investigations
GT 2014; V02AT37A030https://doi.org/10.1115/GT2014-26120
Topics:
Cascades (Fluid dynamics)
,
Clearances (Engineering)
,
Compressors
,
Vortices
,
Wakes
,
Blades
,
Flow (Dynamics)
,
Aerodynamic flow
,
Pressure
,
Probes
Effects of the Steady Wake-Tip Clearance Vortex Interaction in a Compressor Cascade: Part II — Numerical Investigations
GT 2014; V02AT37A031https://doi.org/10.1115/GT2014-26121
Topics:
Cascades (Fluid dynamics)
,
Clearances (Engineering)
,
Compressors
,
Vortices
,
Wakes
,
Flow (Dynamics)
,
Steady state
,
Aerodynamic flow
,
Blades
,
Computation
Bleed-Induced Distortion in Axial Compressors
GT 2014; V02AT37A032https://doi.org/10.1115/GT2014-26195
Topics:
Compressors
,
Flow (Dynamics)
,
Axial flow
,
Ducts
,
Pressure
,
Rotors
,
Stability
Experimental Investigation of Effects of Leading-Edge Tubercles on Compressor Cascade Performance
GT 2014; V02AT37A034https://doi.org/10.1115/GT2014-26242
Topics:
Cascades (Fluid dynamics)
,
Compressors
,
Blades
,
Airfoils
,
Drag (Fluid dynamics)
,
Pressure
,
Axial flow
,
Chords (Trusses)
,
Geometry
,
Probes
Development of a Novel Axial Compressor Generation for Industrial Applications: Part 1 — Compressor Design and Performance
GT 2014; V02AT37A035https://doi.org/10.1115/GT2014-26294
Topics:
Compressors
,
Design
,
Flanges
,
Flow (Dynamics)
,
Power density
,
Pressure
,
Probes
,
Aerodynamics
,
Axial flow
,
Boundary-value problems
Numerical and Experimental Analysis of Radial Clearance Influence on Rotor and Stator Clocking Effect by Example of Model High Loaded Two Stage Compressor
GT 2014; V02AT37A037https://doi.org/10.1115/GT2014-26345
Topics:
Clearances (Engineering)
,
Compressors
,
Experimental analysis
,
Rotors
,
Stators
,
Blades
,
Design
,
Inlet guide vanes
,
Computation
,
Flow (Dynamics)
Investigation of 3D Blading and Non-Axisymmetric Hub Endwall Contouring to a Dual-Stage Counter-Rotating Compressor in Multistage Environment
GT 2014; V02AT37A039https://doi.org/10.1115/GT2014-26450
Topics:
Compressors
,
Optimization
,
Rotors
,
Flow (Dynamics)
,
Flow separation
,
Guide vanes
,
Separation (Technology)
,
Turbines
,
Turbomachinery
,
Vortices
Study on the Effects of Upstream Flow Conditions and Clearance Sizes to Tip Leakage Flow in a Subsonic Large-Scale Rotor
GT 2014; V02AT37A042https://doi.org/10.1115/GT2014-26573
Topics:
Clearances (Engineering)
,
Flow (Dynamics)
,
Leakage flows
,
Rotors
,
Boundary layers
,
Pressure
,
Compressors
,
Design
,
High pressure (Physics)
,
Inflow
Robust Compressor Blades for Desensitizing Operational Tip Clearance Variations
GT 2014; V02AT37A043https://doi.org/10.1115/GT2014-26624
Topics:
Blades
,
Clearances (Engineering)
,
Compressors
,
Design
,
Pressure
,
Uncertainty
,
Computation
,
Engineering design
,
Engineering simulation
,
Leakage flows
Numerical Analysis of Flow in a Transonic Compressor With a Single Circumferential Casing Groove: Application to Two Different Compressor Rotors
GT 2014; V02AT37A044https://doi.org/10.1115/GT2014-26691
Topics:
Compressors
,
Flow (Dynamics)
,
Numerical analysis
,
Rotors
,
Leakage flows
,
Stability
,
Blades
,
Clearances (Engineering)
,
Computational fluid dynamics
,
Design
Investigations on Stator Hub End Losses and its Control in an Axial Flow Compressor
Kurian K. George, S. N. Agnimitra Sunkara, Jubin Tom George, Melvin Joseph, A. M. Pradeep, Bhaskar Roy
GT 2014; V02AT37A047https://doi.org/10.1115/GT2014-26845
Topics:
Axial flow
,
Stators
,
Clearances (Engineering)
,
Blades
,
Rotors
,
Flow (Dynamics)
,
Vortices
,
Design
Visualization and Time Resolved PIV Measurements of the Flow in the Tip Region of a Subsonic Compressor Rotor
GT 2014; V02AT37A051https://doi.org/10.1115/GT2014-27195
Topics:
Compressors
,
Flow (Dynamics)
,
Rotors
,
Visualization
,
Blades
,
Cavitation
,
Vortices
,
Geometry
,
Inlet guide vanes
,
Leakage
A Comparison of Two Fan Stage Designs With Different Rotor Leading Edge Sweep
GT 2014; V02AT37A053https://doi.org/10.1115/GT2014-27218
Topics:
Rotors
,
Stators
,
Pressure
,
Blades
,
Computational fluid dynamics
,
Engines
,
Fans
,
Flow (Dynamics)
,
Stability
,
Temperature
Measurements of the 3D Flow Field Downstream of an Aircraft Engine Fan
GT 2014; V02AT37A054https://doi.org/10.1115/GT2014-27284
Topics:
Aircraft engines
,
Flow (Dynamics)
,
Jet engines
,
Blades
,
Engines
,
Probes
,
Geometry
,
Rotors
,
Wear
,
Clearances (Engineering)
Experimental and Numerical Performance Characterization of a Transonic Compressor Rotor Operating Behind an Inlet-Guide Vane With Variable Flap Angles
GT 2014; V02AT37A056https://doi.org/10.1115/GT2014-27308
Topics:
Compressors
,
Performance characterization
,
Rotors
,
Inlet guide vanes
,
Design
,
Resolution (Optics)
,
Rotation
,
Testing
,
Turbines
Ducts and Component Interactions
An Aggressive S-Shaped Compressor Transition Duct With Swirling Flow and Aerodynamic Lifting Struts
GT 2014; V02AT40A002https://doi.org/10.1115/GT2014-25844
Topics:
Compressors
,
Ducts
,
Swirling flow
,
Struts (Engineering)
,
Momentum
,
Computational fluid dynamics
,
Design
,
Design methodology
,
Flow (Dynamics)
,
Flow separation
Aerodynamic and Heat Transfer Measurements on an Intermediate Turbine Duct Vane
GT 2014; V02AT40A003https://doi.org/10.1115/GT2014-26032
Topics:
Ducts
,
Heat transfer
,
Turbines
,
Computational fluid dynamics
,
Flow (Dynamics)
,
Design
,
Stators
,
Databases
,
Engines
,
Gages
Coupling of Compressible Turbomachinery and Incompressible Combustor Flow Solvers for Aerothermal Applications
GT 2014; V02AT40A004https://doi.org/10.1115/GT2014-26118
Topics:
Combustion chambers
,
Flow (Dynamics)
,
Turbomachinery
,
Computer software
,
Ejectors
,
Gas turbines
,
Guide vanes
,
Simulation
Unsteady Aerodynamics and Forced Response Studies on Aeroderivative Gas Turbine Exhaust System
GT 2014; V02AT40A007https://doi.org/10.1115/GT2014-26989
Topics:
Aerodynamics
,
Exhaust systems
,
Gas turbines
,
Flow (Dynamics)
,
Diffusers
,
Stress
,
Turbulence
,
Vibration
,
Diffusion (Physics)
,
Energy generation
Aerodynamic Design of S-Shaped Diffusers Using Ball Spine Inverse Design Method
GT 2014; V02AT40A008https://doi.org/10.1115/GT2014-27029
Topics:
Design
,
Design methodology
,
Diffusers
,
Ducts
,
Algorithms
,
Flow (Dynamics)
,
Geometry
,
Pressure
,
Separation (Technology)
,
Turbulence
Noise and Innovative Noise Reduction (With Aircraft Engine)
Applying an Extended Non Linear Harmonic Method to a CROR Configuration With Emphasis on the Acoustic Signature
GT 2014; V02AT41A001https://doi.org/10.1115/GT2014-25061
Topics:
Acoustics
,
Rotors
,
Aircraft
,
Blades
,
Computational fluid dynamics
,
Fluctuations (Physics)
,
Pressure
,
Stress
,
Design
,
Fans
Effect of Airfoil Clocking on Noise of LP Turbines: Part II — Modal Structure Analysis
GT 2014; V02AT41A003https://doi.org/10.1115/GT2014-25602
Topics:
Airfoils
,
Noise (Sound)
,
Turbines
,
Acoustics
,
Ducts
,
Spin (Aerodynamics)
,
Spinning (Textile)
,
Engines
,
Pressure
,
Rotation
Acoustic Design and Validation of Radial Inflow Turbine
GT 2014; V02AT41A004https://doi.org/10.1115/GT2014-25935
Topics:
Acoustics
,
Design
,
Inflow
,
Turbines
,
Noise (Sound)
,
Rotors
,
Testing
,
Computational fluid dynamics
,
Sound pressure
Computational Study on Acoustic Features of Fan Model With Leaned Stators
GT 2014; V02AT41A006https://doi.org/10.1115/GT2014-26350
Topics:
Acoustics
,
Stators
,
Noise (Sound)
,
Aviation
,
Motors
,
Rotation
,
Rotors
,
Test facilities
Numerical Investigation of High Bypass Ratio Fan Tone Noise
GT 2014; V02AT41A007https://doi.org/10.1115/GT2014-26354
Topics:
Noise (Sound)
,
Acoustics
,
Simulation
,
Anechoic chambers
,
Computation
,
Test facilities
,
Turbojets
Prediction of the Aero-Acoustic Performance of Open Rotors
GT 2014; V02AT41A008https://doi.org/10.1115/GT2014-26413
Topics:
Acoustics
,
Rotors
,
Noise (Sound)
,
Wake turbulence
,
Wakes
,
Blades
,
Design methodology
,
Jet fuels
,
Particulate matter
,
Propulsion systems
Integrated “CFD - Acoustic” Computational Approach to the Simulation of Aircraft Fan Noise
Piergiorgio Ferrante, Paolo di Francescantonio, Pierre-Alain Hoffer, Stéphane Vilmin, Charles Hirsch
GT 2014; V02AT41A009https://doi.org/10.1115/GT2014-26429
Topics:
Acoustics
,
Aircraft
,
Computational fluid dynamics
,
Noise (Sound)
,
Simulation
,
Boundary element methods
,
Unsteady flow
,
Ducts
,
Engines
,
Finite element methods
CFD Analysis of the Aerodynamics and Aeroacoustics of the NASA SR2 Propeller
GT 2014; V02AT41A010https://doi.org/10.1115/GT2014-26779
Topics:
Aerodynamic noise
,
Aerodynamics
,
Computational fluid dynamics
,
NASA
,
Propellers
,
Noise (Sound)
,
Blades
,
Wakes
,
Convection
,
Simulation
Full-Scale Tests on APU Noise Reduction
GT 2014; V02AT41A011https://doi.org/10.1115/GT2014-26803
Topics:
Noise control
,
Emissions
,
Exhaust systems
,
Noise (Sound)
,
Silencers
,
Aircraft
,
Control systems
,
Engines
,
Microphones
Aerodynamic and Aeroacoustic Optimization of a Transonic Centrifugal Compressor
GT 2014; V02AT41A012https://doi.org/10.1115/GT2014-26813
Topics:
Compressors
,
Optimization
,
Design
,
Noise (Sound)
,
Blades
,
Computational fluid dynamics
,
Flow (Dynamics)
,
Diffusers
,
Engineering simulation
,
Pressure
A High-Resolution, Continuous-Scan Acoustic Measurement Method for Turbofan Engine Applications
GT 2014; V02AT41A013https://doi.org/10.1115/GT2014-27108
Topics:
Acoustics
,
Engines
,
Resolution (Optics)
,
Turbofans
,
Microphones
,
Noise (Sound)
,
Signals
,
Data acquisition
,
Electromagnetic scattering
,
Filters
Effect of Blade Tip Modifications for Unducted Propulsors on Tip Vortex-Rotor Interaction Noise
GT 2014; V02AT41A014https://doi.org/10.1115/GT2014-27134
Topics:
Blades
,
Noise (Sound)
,
Rotors
,
Vortices
,
Acoustic emissions
,
Acoustics
,
Computational fluid dynamics
,
Emissions
,
Navier-Stokes equations
,
Pressure