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    An Argument for Enhancement of the Current Inlet Distortion Ground Test Practice for Aircraft Gas Turbine Engines1 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 002:;page 235
    Author(s): Milt Davis; Alan Hale; Dave Beale
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The current high-performance aircraft development programs, and the trends in research and development activities suggest a rapidly increasing level of aircraft subsystem integration, particularly ...
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    A Numerical Simulation Capability for Analysis of Aircraft Inlet-Engine Compatibility 

    Source: Journal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 003:;page 473
    Author(s): Alan Hale; Milt Davis; Jim Sirbaugh
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Two primary aircraft propulsion subsystems are the inlet and the engine. Traditionally these subsystems have been designed, analyzed, and tested as isolated systems. The interaction between the ...
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    An Investigation Into the Effects of Highly Transient Flight Maneuvers With Heat and Mass Transfer on the T-38 Air Force Trainer Inlet 

    Source: Journal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 003:;page 31201
    Author(s): Alan Hale; Andrew Hughes; Jim Sirbaugh; David S. Kidman
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The T-38 talon currently serves as the primary United States Air Force trainer for fighter aircraft. This supersonic trainer was developed in the 1960s but continues to be used today as the ...
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