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    High Lift and Aft-Loaded Profiles for Low-Pressure Turbines 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 002:;page 181
    Author(s): R. J. Howell; N. W. Harvey; V. Schulte; O. N. Ramesh; H. P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper shows how it is possible to reduce the number of blades in LP turbines by approximately 15 percent relative to the first generation of high lift blading employed in the very ...
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    Development of Blade Profiles for Low-Pressure Turbine Applications 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 003:;page 531
    Author(s): E. M. Curtis; N. W. Harvey; H. P. Hodson; M. R. Banieghbal; J. D. Denton; R. J. Howell
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a program of work, largely experimental, which was undertaken with the objective of developing an improved blade profile for the low-pressure turbine in aero-engine applications. ...
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    Boundary Layer Development in the BR710 and BR715 LP Turbines—The Implementation of High-Lift and Ultra-High-Lift Concepts 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 003:;page 385
    Author(s): R. J. Howell; Heinz-Peter Schiffer; N. W. Harvey; F. Haselbach; H. P. Hodson; V. Schulte; R. D. Stieger
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a detailed study into the unsteady boundary layer behavior in two high-lift and one ultra-high-lift Rolls-Royce Deutschland LP turbines. The objectives of the paper are to ...
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