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    Conceptual design studies of lift/cruise fans for military transports (1974)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: A study program for conceptual design studies of remote lift and lift/cruise fan systems to meet the requirements of military V/STOL aircraft was conducted. Parametric performance and design data are presented for fans covering a range of pressure ratios, including both single and two stage fan concepts. The gas generator selected for these fan systems was the J101-GE-100 engine. Noise generation and transient response were determined for selected fan systems.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-CR-134636 , R74AEG283
    Format: application/pdf
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