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    Multistage Turbine Simulations With Vortex–Blade Interaction 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 004:;page 643
    Author(s): M. G. Turner
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The average passage approach of Adamczyk et al. (1990) has been used to simulate the multistage environment of the General Electric E3 low-pressure turbine. Four configurations have been analyzed ...
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    Three-Dimensional Navier–Stokes Computations of Transonic Fan Flow Using an Explicit Flow Solver and an Implicit κ–ε Solver 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 002:;page 261
    Author(s): I. K. Jennions; M. G. Turner
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Computational fluid dynamics (CFD) has become a powerful ally of the experimental test facility in revealing the flow physics of some highly complex flows. For certain classes of flow, CFD has ...
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    An Investigation of Turbulence Modeling in Transonic Fans Including a Novel Implementation of an Implicit k–ε Turbulence Model 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 002:;page 249
    Author(s): M. G. Turner; I. K. Jennions
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An explicit Navier–Stokes solver has been written with the option of using one of two types of turbulence model. One is the Baldwin–Lomax algebraic model and the other is an implicit k –ε ...
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    Compressor Blade Forced Response Due to Downstream Vane-Strut Potential Interaction 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 001:;page 134
    Author(s): H.-W. D. Chiang; M. G. Turner
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A blade forced response prediction system has been developed using an implicit two-dimensional CFD solver to model the rotor blade forced response due to the static pressure distortion (potential ...
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