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    Future Use of Large Eddy Simulation in Aeroâ€گengines 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 008:;page 81005
    Author(s): Tyacke, James C.; Tucker, Paul G.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Computational fluid dynamics (CFD) has become a critical tool in the design of aeroengines. Increasing demand for higher efficiency, performance, and reduced emissions of noise and pollutants has focused attention on ...
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    Modular Turbulence Modeling Applied to an Engine Intake 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 005:;page 51004
    Author(s): Oriji, Ugochukwu R.; Tucker, Paul G.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The one equation Spalart–Allmaras (SA) turbulence model in an extended modular form is presented. It is employed for the prediction of crosswind flow around the lip of a 90 deg sector of an intake with and without ...
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    Differential Equation Specification of Integral Turbulence Length Scales 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 003:;page 31013
    Author(s): Jefferson; Tucker, Paul G.; Northall, John D.; Nagabhushana Rao, V.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A Hamilton–Jacobi differential equation is used to naturally and smoothly (via Dirichlet boundary conditions) set turbulence length scales in separated flow regions based on traditional expected length scales. Such zones ...
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    Numerical Investigation of Three-Dimensional Separation in an Axial Flow Compressor: The Influence of Freestream Turbulence Intensity and Endwall Boundary Layer State 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 002:;page 21011
    Author(s): Scillitoe, Ashley D.; Tucker, Paul G.; Adami, Paolo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Regions of three-dimensional separations are an inherent flow feature of the suction surface-endwall corner in axial compressors. These corner separations can cause a significant total pressure loss and reduce the compressor's ...
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    RANS Modeling of Accelerating Boundary Layers 

    Source: Journal of Fluids Engineering:;2015:;volume( 137 ):;issue: 001:;page 11202
    Author(s): Oriji, Ugochukwu R.; Karimisani, Sahand; Tucker, Paul G.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A numerical investigation of accelerated boundary layers (BL) has been performed using linear and nonlinear eddy viscosity models (EVM). The acceleration parameters (KS) investigated the range between 1.5 أ— 10−6 and ...
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    Inverse Design of 3D Multistage Transonic Fans at Dual Operating Points 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 004:;page 41008
    Author(s): Page, James H.; Hield, Paul; Tucker, Paul G.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Semiinverse design is the automatic recambering of an aerofoil during a computational fluid dynamics (CFD) calculation in order to achieve a target lift distribution while maintaining thickness, hence, “semiinverse.â€‌ ...
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    Effect of Inlet Distortion Features on Transonic Fan Rotor Stall 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 007:;page 71008
    Author(s): Page, James H.; Hield, Paul; Tucker, Paul G.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of inlet distortion from curved intake ducts on jet engine fan stability is an important consideration for next-generation passenger aircraft such as the boundary layer ingestion (BLI) “silent aircraft.” Highly ...
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    Large Eddy Simulation of Boundary Layer Transition Mechanisms in a Gas-Turbine Compressor Cascade 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 006:;page 61008
    Author(s): Scillitoe, Ashley D.; Tucker, Paul G.; Adami, Paolo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Large eddy simulation (LES) is used to explore the boundary layer transition mechanisms in two rectilinear compressor cascades. To reduce numerical dissipation, a novel locally adaptive smoothing (LAS) scheme is added to ...
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    Toward Future Installations: Mutual Interactions of Short Intakes With Modern High Bypass Fans 

    Source: Journal of Turbomachinery:;2019:;volume 141:;issue 008
    Author(s): Vadlamani, Nagabhushana Rao; Cao, Teng; Watson, Rob; Tucker, Paul G.
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, we investigate the coupled interaction between a new short intake design with a modern fan in a high-bypass ratio civil engine, specifically under the off-design condition of high incidence. The interaction ...
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    Numerical Analysis of an Instrumented Turbine Blade Cascade 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 05:;page 51013
    Author(s): Ubald, Bryn N.; Tucker, Paul G.; Cui, Jiahuan; Watson, Rob; Shahpar, Shahrokh
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The measurement accuracy of the temperature/pressure probe mounted at the leading edge of a turbine/compressor blade is crucial for estimating the fuel consumption of a turbo-fan engine. Apart from the measurement error ...
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