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  • Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems. Task 8, Cooling flow/heat transfer analysis [microform] : users manual / E.J. Hall ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Anaylsis of interior noise ground and flight test data for advanced turboprop aircraft applications [microform] / M.A. Simpson and B.N. Tran.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Structural Tailoring of Advanced Turboprops (STAT) [microform] : programmer's manual / K.W. Brown [and] P.R. Harvey.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers [microform] / George L. Stefko and Robert J. Jeracki.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications [microform] / Paul L. McDill.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Advanced turboprop wing installation effects measured by unsteady blade pressure and noise [microform] / Laurence J. Heidelberg and Richard P. Woodward ; prepared for the 11th Aeroacoustics Conference sponsored by the American Institute of Aeronautics and Astronautics, Sunnyvale, California, October 19-21, 1987.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Experimental classical flutter results of a composite advanced turboprop model [microform] / O. Mehmed and K.R.V. Kaza.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • A review of propeller noise prediction methodology 1919-1994 [microform] / F. Bruce Metzger.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Advanced gearbox technology [microform] : final report / by N. E. Anderson, ... [et al.].

    • Text
    • [Cleveland, Ohio] : NASA Lewis Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60952

  • A numerical simulation of the inviscid flow through a counter-rotating propeller [microform] / Mark L. Celestina, Richard A. Mulac, and John J. Adamczyk.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • Comparison of advanced turboprop and conventional jet and propeller aircraft flyover noise annoyance [microform] : preliminary results / David A. McCurdy.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS85579

  • Low-speed wind-tunnel tests of single- and counter-rotation propellers [microform] / Dana Morris Dunham, Garl L. Gentry, Jr., and Paul L. Coe, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986.
    • 1986

  • Analytical fuel property effects. Small combustors. Phase 2 [microform] : final report / by T.G. Hill, J.D. Monty and H.L. Morton; prepared for National Aeronautics and Space Administration, Lewis Research Center.

    • Text
    • Lynn, MA : Aircraft Engine Business Group, General Electric, [1985]
    • 1985

  • Analysis and test evaluation of the dynamic stability of three advanced turboprop models at zero forward speed / by Arthur F. Smith.

    • Text
    • Windsor Locks, Conn. : Hamilton Standard Division, United Technologies Corporation ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo26015

  • Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed [microform] / by Arthur F. Smith.

    • Text
    • Windsor Locks, Conn. : United Technologies Corporation, Hamilton Standard Division ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service], 1985.
    • 1985

  • Piloted simulation study of an ILS approach of a twin-pusher business/commuter turboprop aircraft configuration / Donald R. Riley and Jay M. Brandon, Louis J. Glaab.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 1994.
    • 1994-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo157689

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