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    Oscillatory Flow in a Physical Model of a Thin Slab Casting Mould With a Bifurcated Submerged Entry Nozzle 

    Source: Journal of Fluids Engineering:;2002:;volume( 124 ):;issue: 002:;page 535
    Author(s): Nicholas J. Lawson; Lecturer; Malcolm R. Davidson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Laser Doppler anemometry (LDA) measurements are presented of the oscillatory flow in a 33% scale water model of thin slab casting mould when the flow enters as two lateral jets through a ...
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    Crossflow Characteristics of an Oscillating Jet in a Thin Slab Casting Mould 

    Source: Journal of Fluids Engineering:;1999:;volume( 121 ):;issue: 003:;page 588
    Author(s): Nicholas J. Lawson; Malcolm R. Davidson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The application of LDA to a transient 1/3 scale (500 mm wide) water model of a mould, typical of steel thin slab casting, is presented. The characteristics of a crossflow, associated with ...
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    Application of Optical Measurement Techniques to Supersonic and Hypersonic Aerospace Flows 

    Source: Journal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 004
    Author(s): David Estruch; Nicholas J. Lawson; Kevin P. Garry
    Publisher: American Society of Civil Engineers
    Abstract: Experimental investigation is essential to improve the understanding of aerospace flows. During the last years, effort has been put on the development of optical diagnostics capable of imaging or yielding data from the ...
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    DES of a Slingsby Firefly Aircraft: Unsteady Flow Feature Extraction Using POD and HODMD 

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 005:;page 04022063
    Author(s): Adrián Corrochano; Ana F. Neves; Bidur Khanal; Soledad Le Clainche; Nicholas J. Lawson
    Publisher: ASCE
    Abstract: In this paper, higher-order dynamic mode decomposition (HODMD) was applied to find the main patterns and frequencies of a transient aerodynamic flow field when an aircraft wing experiences stall. This method was applied ...
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