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  • Navier-Stokes simulation of the supersonic combustion flowfield in a ram accelerator [microform] / Shaye Yungster.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991

  • Numerical study of shock-induced combustion in methane-air mixtures [microform] / Shaye Yungster and Martin J. Rabinowitz.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Computational study of single-expansion-ramp nozzles with external burning [microform] / Shaye Yungster and Charles J. Trefny.

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

  • A fully implicit time accurate method for hypersonic combustion [microform] : application to shock-induced combustion instability / Shaye Yungster and Krishnan Radhakrishnan.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Application of chimera grid scheme to combustor flowfields at all speeds [microform] / Shaye Yungster, Kuo-Huey Chen.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Computational study of near-limit propagation of detonation in hydrogen-air mixtures [microform] / S. Yungster and K. Radhakrishnan.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Hanover, MD : Available from MASA Center for Aerospace Information, [2002]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS36060

  • Multiple-cycle simulation of a pulse detonation engine ejector [microform] / S. Yungster [and] H.D. Perkins.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS53266

  • Computational study of near-limit propagation of detonation in hydrogen-air mixtures [microform] / S. Yungster, K. Radhakrishnan.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va.: For sale by the National Technical Information Service, 2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60236

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