Research Catalog

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  • Full Navier-Stokes analysis of a two-dimensional mixer/ejector nozzle for noise suppression [microform] / James R. DeBonis.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
    • 1992

  • A method for flow simulation about complex geometries using both structured and unstructured grids [microform] / James R. DeBonis.

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

  • Validation of the NPARC code for nozzle afterbody flows at transonic speeds [microform] / James R. DeBonis and Nicholas J. Georgiadis, Crawford F. Smith.

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

  • The numerical analysis of a turbulent compressible jet [microform] / James R. DeBonis.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26824

  • Rocket-based combined cycle engine technology development : inlet CFD validation and application / J.R. DeBonis and S. Yungster.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1996.
    • 1996-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69485

  • Prediction of turbulent temperature fluctuations in hot jets / James R. DeBonis.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2017.
    • 2017-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo84063

  • Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system / J.R. DeBonis and C.J. Trefny.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2001.
    • 2001-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS23166

  • The numerical analysis of a turbulent compressible jet / James R. DeBonis.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2001.
    • 2001-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS26824

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