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    Satellite-Derived Surface Energy Balance Estimates in the Alaskan Sub-Arctic 

    Source: Journal of Climate and Applied Meteorology:;1983:;volume( 022 ):;issue: 001:;page 115
    Author(s): Gurney, R. J.; Hall, D. K.
    Publisher: American Meteorological Society
    Abstract: Heat Capacity Mapping Mission (HCMM) data for 12 May 1978 were used in an energy balance modelto estimate evapotranspiration in sub-Arctic Alaska following snowmelt. The HCMM scene contained severalareas of melting snow ...
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    Analysis of Fan Stage Conceptual Design Attributes for Boundary Layer Ingestion 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 007:;page 71012
    Author(s): Hall, D. K.; Greitzer, E. M.; Tan, C. S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a new conceptual framework for three-dimensional turbomachinery flow analysis and its use to assess fan stage attributes for mitigating adverse effects of inlet distortion due to boundary layer ingestion ...
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    Fan Performance Scaling With Inlet Distortions 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 007:;page 71009
    Author(s): Defoe, J. J.; Etemadi, M.; Hall, D. K.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Applications such as boundary-layer-ingesting (BLI) fans and compressors in turboprop engines require continuous operation with distorted inflow. A low-speed axial fan with incompressible flow is studied in this paper. The ...
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    Mitigation of Boundary Layer Ingestion Circumferential Distortion Using Nonaxisymmetric Fan Exit Guide Vanes 

    Source: Journal of Turbomachinery:;2022:;volume( 145 ):;issue: 003:;page 31008-1
    Author(s): Hall, D. K.; Greitzer, E. M.; Tan, C. S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents an assessment of the effect of nonaxisymmetric fan exit guide vanes (FEGVs) to mitigate, or even reduce to zero, the impact of circumferential flow distortion—such as created by boundary layer ingestion ...
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    Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation 

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 010:;page 101002-1
    Author(s): Hall, D. K.; Greitzer, E. M.; Uranga, A.; Drela, M.; Pandya, S. A.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article presents first-of-a-kind measurements, and complementary computations, of the flow through the propulsion system of a boundary layer ingesting, twin-engine advanced civil transport aircraft configuration. The ...
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