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    Steady Performance Measurements of a Turbofan Engine With Inlet Distortions Containing Co- and Counterrotating Swirl From an Intake Diffuser for Hypersonic Flight 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 002:;page 379
    Author(s): Norbert R. Schmid; Dirk C. Leinhos; Leonhard Fottner
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The influence of distorted inlet flow on the steady and unsteady performance of a turbofan engine, which is a component of an air-breathing combined propulsion system for a hypersonic transport ...
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    The Influence of Transient Inlet Distortions on the Instability Inception of a Low-Pressure Compressor in a Turbofan Engine 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 001:;page 1
    Author(s): Dirk C. Leinhos; Norbert R. Schmid; Leonhard Fottner
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: While studies on compressor flow instabilities under the presence of inlet distortions have been carried out with steady distortions in the past, the investigation presented here focuses on the ...
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