Technology readiness for Mach 0.7 to 0.8 turboprop powered aircraft with the potential for fuel savings and DOC reductions of up to 30 and 15 percent respectively relative to current in-service aircraft is addressed. The areas of propeller aeroacoustics, propeller structures, turboprop installed performance, aircraft cabin environment, and turboprop engine and aircraft studies are emphasized. Large scale propeller characteristics and high speed propeller flight research tests using a modified testbed aircraft are also considered.


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    Titel :

    The NASA High-Speed Turboprop Program


    Beteiligte:
    J. F. Dugan (Autor:in) / B. A. Miller (Autor:in) / E. J. Graber (Autor:in) / D. A. Sagerser (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    48 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    The NASA High-Speed Turboprop Program

    Miller, Brent A. / Sagerser, David A. / Graber, Edwin J. et al. | SAE Technical Papers | 1980


    The NASA high-speed turboprop program

    Dugan, J. F. / Miller, B. A. / Graber, E. J. et al. | NTRS | 1980


    The NASA high-speed turboprop program

    Dugan, J. F. / Miller, B. A. / Graber, E. J. et al. | NTRS | 1980


    NASA/industry advanced turboprop technology program

    Ziemianski, Joseph A. / Whitlow, John B., Jr. | NTRS | 1988


    NASA/industry advanced turboprop technology program

    Ziemianski, Joseph A. / Whitlow, John B., Jr. | NTRS | 1988