Research Catalog

  • Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at mach 0.2 [microform] / D. R. Boldman ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991
  • Aeroacoustic diffraction and dissipation by a short propeller cowl in subsonic flight [microform] / Rudolph Martinez.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993
  • Advanced nacelle acoustic lining concepts development [microform] / G. Bielak ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60573
  • Effect of a rotating propeller on the separation angle of attack and distortion in ducted propeller inlets [microform] / D. R. Boldman, ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, [1992?]
    • 1992
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97761
  • Acoustic mode measurements in the inlet of a model turbofan using a continuously rotating rake [microform] / Laurence J. Heidelberg and David G. Hall.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration, 1992]
    • 1992

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