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    Discussion: “Quasi-Three-Dimensional and Full Three-Dimensional Rotational Flow Calculations in Turbomachines” (Wang, Qinghuan, Zhu, Genxing, and Wu, Chung-Hua, 1985, ASME J. Eng. Gas Turbines Power, 107, pp. 277–284) 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 002:;page 284
    Author(s): I. K. Jennions
    Publisher: The American Society of Mechanical Engineers (ASME)
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    A Quasi-Three-Dimensional Turbomachinery Blade Design System: Part II—Computerized System 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 002:;page 308
    Author(s): I. K. Jennions; P. Stow
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The purpose of this work has been to develop a quasi-three-dimensional blade design and analysis system. In Part II of the paper the computerized blade design system is presented and an example ...
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    A Quasi-Three-Dimensional Turbomachinery Blade Design System: Part I—Throughflow Analysis 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 002:;page 301
    Author(s): I. K. Jennions; P. Stow
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The purpose of this work has been to develop a quasi-three-dimensional blade design and analysis system incorporating fully linked throughflow, blade-to-blade and blade section stacking programs. ...
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    The Importance of Circumferential Non-uniformities in a Passage-Averaged Quasi-Three-Dimensional Turbomachinery Design System 

    Source: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 002:;page 240
    Author(s): I. K. Jennions; P. Stow
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The purpose of this paper is to show, for both rotating and non-rotating blade rows, the importance of including circumferential non-uniform flow effects in a quasi-three-dimensional blade design ...
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    Evaluation of the Interaction Losses in a Transonic Turbine HP Rotor/LP Vane Configuration 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 001:;page 68
    Author(s): I. K. Jennions; J. J. Adamczyk
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Transonic turbine rotors produce shock waves, wakes, tip leakage flows, and other secondary flows that the downstream stators have to ingest. While the physics of wake ingestion and shock ...
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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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    The Computation of Adjacent Blade-Row Effects in a 1.5-Stage Axial Flow Turbine 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 001:;page 1
    Author(s): R. Emunds; I. K. Jennions; D. Bohn; J. Gier
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper deals with the numerical simulation of flow through a 1.5-stage axial flow turbine. The three-row configuration has been experimentally investigated at the University of Aachen where ...
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