Research Catalog

New! Try our Article Search to discover online journals, books, and more from home with your library card.

Selected filters.Clear Filters

  • In flight measurement of steady and unsteady blade surface pressure of a single rotation large scale advanced prop-fan installed on the PTA aircraft [microform] / D. Parzych ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; 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

  • Advanced turboprop aircraft flyover noise [microform] : annoyance to counter-rotating-propeller configurations with an equal number of blades on each rotor : preliminary results / David A. McCurdy.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va.? : National Technical Information Service, distributor, 1988]
    • 1988

  • Dynamic response and stability of a composite prop-fan model [microform] / by Arthur F. Smith and Bennett M. Brooks.

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

  • An experimental investigation of the interior noise control effects of propeller synchrophasing [microform] / J.D. Jones and C.R. Fuller.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986

  • Large-scale advanced prop-fan (LAP) hub/blade retention design report [microform] / by Matthew Soule.

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

  • Development and validation of a blade-element mathematical model for the AH-64A Apache helicopter [microform] / M. Hossein Mansur.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • 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

  • Effect of angular inflow on the vibratory response of a counter-rotating propeller [microform] : by J.E. Turnberg, P.C. Brown.

    • Text
    • [Washington, DC] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1985]
    • 1985

  • 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

  • An integrated optimum design approach for high speed prop rotors [microform] : final report on NASA Ames grant no. NCC2-795 / Chattopadhyay and Thomas R. McCarthy.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Optical measurement of propeller blade deflections [microform] / Anatole P. Kurkov.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1988.
    • 1988

  • Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack [microform] / M. Nallasamy and J.F. Groeneweg.

    • Text
    • Cleveland, Ohio : Lewis Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58503

  • Effect of reduced aft diameter and increased blade number on high-speed counterrotation propeller performance [microform] / Gayle E. Rose, Robert J. Jeracki.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS61130

  • Unsteady potential flow past a propeller blade section [microform] / M.A. Takallu.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65495

  • Acoustic and aerodynamic study of a pusher-propeller aircraft model [microform] / Paul T. Soderman and W. Clifton Horne.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67790

  • Application of an efficient hybrid scheme for aeroelastic analysis of advanced propellers [microform] / R. Srivastava ... [et al.] ; prepared for the 28th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 8-11, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70410

  • Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A [microform] / James H. Dittmar.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1985]
    • 1985

  • 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

  • Model helicopter rotor high-speed impulsive noise [microform] : measured acoustics and blade pressures / D. A. Boxwell ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS89480

  • Large-scale advanced prop-fan (LAP) blade design [microform] / by: William E. Sullivan, Jay E. Turnberg, John A. Violette.

    • Text
    • [Windsor Locks, Conn.?] : Hamilton Standard Division, United Technologies ; [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1984?]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS89211

  • Flow field survey near the rotational plane of an advanced design propeller on a Jetstar airplane [microform] / Kevin Robert Walsh.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1985.
    • 1985

  • Noise of the SR-6 propeller model at 2⁰ and 4⁰ angles of attack [microform] / James H. Dittmar, George L. Stefko, and Robert J. Jeracki.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1983]
    • 1983

  • Vortex conception of rotor and mutual effect of screw/propellers [microform] / A.M. Lepilkin.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1986]
    • 1986

  • Profile design for wings and propellers [microform] / A. Quast and K.H. Horstmann.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1984]
    • 1984

  • Noise constraints effecting optimal propeller designs / Christopher J. Miller and John P. Sullivan.

    • Text
    • [Wasington, D.C.] : National Aeronautics and Space Administration, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS105616

  • Noise constraints effecting optimal propeller designs [microform] / Christopher J. Miller and John P. Sullivan.

    • Text
    • [Wasington, D.C.] : National Aeronautics and Space Administration, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS105616

  • Optical measurement of propeller blade deflections in a spin facility / John K. Ramsey, ... [and others].

    • Text
    • [Cleveland, Ohio] : [Lewis Research Center], [1990]
    • 1990
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS60522

  • Aerodynamic design of a propeller for high-altitude balloon trajectory control / Richard Eppler and Dan M. Somers.

    • Text
    • Greenbelt, Maryland : National Aeronautics and Space Administration, Goddard Space Flight Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo38352

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta