Research Catalog

  • Flow analysis for the nacelle of an advanced ducted propeller at high angle-of-attack and at cruise with boundary layer control [microform] / D.P. Hwang, D.R. Boldman, and C.E. Hughes.

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

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