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Issues
October 2019
ISSN 0889-504X
EISSN 1528-8900
SPECIAL ISSUE: 15TH INTERNATIONAL SYMPOSIUM ON UNSTEADY AERODYNAMICS, AEROACOUSTICS AND AEROELASTICITY OF TURBOMACHINERY (ISUAAAT15)
ISUAAAT15 Special Issue
J. Turbomach. October 2019, 141(10): 100201.
doi: https://doi.org/10.1115/1.4044448
Investigation of the Impact of Unsteady Turbulence Effects on the Aeroelastic Analysis of a Low-Pressure Turbine Rotor Blade
J. Turbomach. October 2019, 141(10): 100801.
doi: https://doi.org/10.1115/1.4043950
Topics:
Blades
,
Filters
,
Pressure
,
Rotors
,
Simulation
,
Turbulence
,
Flow (Dynamics)
Coupled Fan–Stator Aerodynamic and Acoustic Response to Inflow Distortion
J. Turbomach. October 2019, 141(10): 101001.
doi: https://doi.org/10.1115/1.4043963
Topics:
Acoustics
,
Stators
,
Waves
,
Electromagnetic scattering
,
Radiation scattering
,
Scattering (Physics)
,
S-matrix theory
,
Inflow
,
Wakes
,
Blades
Rotor–Stator Interactions in a 2.5-Stage Axial Compressor—Part I: Experimental Analysis of Tyler–Sofrin Modes
J. Turbomach. October 2019, 141(10): 101002.
doi: https://doi.org/10.1115/1.4043961
Topics:
Blades
,
Compressors
,
Pressure
,
Rotors
,
Stators
,
Stress
,
Pressure measurement
,
Signals
Rotor–Stator Interactions in a 2.5-Stage Axial Compressor—Part II: Impact of Aerodynamic Modeling on Forced Response
J. Turbomach. October 2019, 141(10): 101008.
doi: https://doi.org/10.1115/1.4043954
Topics:
Acoustics
,
Blades
,
Compressors
,
Excitation
,
Pressure
,
Rotors
,
Simulation
,
Stators
,
Stress
,
Inlet guide vanes
CFD-Aided Design of a Transonic Aeroelastic Compressor Rig
J. Turbomach. October 2019, 141(10): 101003.
doi: https://doi.org/10.1115/1.4043884
Topics:
Blades
,
Compressors
,
Computational fluid dynamics
,
Design
,
Flow (Dynamics)
,
Mach number
,
Optimization
,
Pressure
,
Simulation
,
Geometry
Project PHARE-2—A High-Speed UHBR Fan Test Facility for a New Open-Test Case
Christoph Brandstetter, Valdo Pages, Pierre Duquesne, Benoit Paoletti, Stéphane Aubert, Xavier Ottavy
J. Turbomach. October 2019, 141(10): 101004.
doi: https://doi.org/10.1115/1.4043883
Tonal Fan-Noise Radiation From Aero-Engine Bypass With Serrated End Treatments
J. Turbomach. October 2019, 141(10): 101005.
doi: https://doi.org/10.1115/1.4043882
Tip-Shroud Labyrinth Seal Effect on the Flutter Stability of Turbine Rotor Blades
J. Turbomach. October 2019, 141(10): 101006.
doi: https://doi.org/10.1115/1.4043962
Topics:
Airfoils
,
Blades
,
Cavities
,
Damping
,
Flow (Dynamics)
,
Flutter (Aerodynamics)
,
Pressure
,
Rotors
,
Stability
,
Turbines
On the Influence of Blade Aspect Ratio on Aerodynamic Damping
J. Turbomach. October 2019, 141(10): 101007.
doi: https://doi.org/10.1115/1.4043905
Topics:
Blades
,
Damping
,
Simulation
,
Computational fluid dynamics
,
Rotors
,
Traveling waves
Machine-Learnt Turbulence Closures for Low-Pressure Turbines With Unsteady Inflow Conditions
J. Turbomach. October 2019, 141(10): 101009.
doi: https://doi.org/10.1115/1.4043907
Topics:
Errors
,
Flow (Dynamics)
,
Physics
,
Turbulence
,
Wakes
,
Inflow
,
Approximation
,
Locks (Waterways)
,
Model development
,
Pressure
Study of the Effect of the Scatter of Acoustic Modes on Turbine Flutter
J. Turbomach. October 2019, 141(10): 101010.
doi: https://doi.org/10.1115/1.4043909
Topics:
Acoustics
,
Flutter (Aerodynamics)
,
Waves
,
Simulation
,
Reflection
,
Electromagnetic scattering
,
Turbines
Radial Decomposition of Blade Vibration to Identify a Stall Flutter Source in a Transonic Fan
J. Turbomach. October 2019, 141(10): 101011.
doi: https://doi.org/10.1115/1.4044484
Topics:
Blades
,
Flutter (Aerodynamics)
,
Pressure
,
Shock waves
,
Vibration
,
Fluctuations (Physics)
,
Flow (Dynamics)
,
Damping
,
Computation
,
Oscillations
Effect of Geometric Variability on Running Shape and Performance of a Transonic Fan
J. Turbomach. October 2019, 141(10): 101012.
doi: https://doi.org/10.1115/1.4044676
Topics:
Blades
,
Computation
,
Manufacturing
,
Stiffness
,
Geometry
Non-Synchronous Aeroacoustic Interaction in an Axial Multi-Stage Compressor
J. Turbomach. October 2019, 141(10): 101013.
doi: https://doi.org/10.1115/1.4044675
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