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    Poststall Behavior of a Multistage High Speed Compressor at Off-Design Conditions 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 012:;page 121002
    Author(s): Zhao, Fanzhou; Dodds, John; Vahdati, Mehdi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Stall followed by surge in a high speed compressor can lead to violent disruption of flow, damage to the blade structures and, eventually, engine shutdown. Knowledge of unsteady blade loading during such events is crucial ...
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    Flow Physics During Surge and Recovery of a Multi-Stage High-Speed Compressor 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 006:;page 061008-1
    Author(s): Zhao, Fanzhou; Dodds, John; Vahdati, Mehdi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Stall followed by surge in a high-speed compressor can lead to violent disruption of the flow, damage to the blade structures and eventually engine shutdown. Knowledge of unsteady blade loading during surge is crucial for ...
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    Validation of a Numerical Model for Predicting Stalled Flows in a Low-Speed Fan—Part II: Unsteady Analysis 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 005:;page 51009
    Author(s): Lee, Kuen-Bae; Dodds, John; Wilson, Mark; Vahdati, Mehdi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper investigates the flow near the stall boundary for a low-speed/low-pressure ratio fan. Three-dimensional, Reynolds-averaged Navier–Stokes computations are performed for a modern low speed fan rig for which extensive ...
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    Deficiencies in the Spalart–Allmaras Turbulence Model for the Prediction of the Stability Boundary in Highly Loaded Compressors 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 012:;page 0121012-1
    Author(s): Moreno, Jose; Dodds, John; Stapelfeldt, Sina; Vahdati, Mehdi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Reynolds-averaged Navier–Stokes (RANS) equations are employed for aerodynamic and aeroelastic modeling in axial compressors. Their solutions are highly dependent on the turbulence models for closure. The main objective of ...
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    Aerodynamic Loading Considerations of Three-Shaft Engine Compression System During Surge 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 012:;page 0121002-1
    Author(s): Moreno, Jose; Dodds, John; Sheaf, Christopher; Zhao, Fanzhou; Vahdati, Mehdi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Compressor surge imposes a limit on aero-engine operability and can compromise integrity because of significant aerodynamic loads imparted on the engine components. The aim of this article is to use 3D unsteady computational ...
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