Research Catalog

  • Implications of adhesion studies for dust mitigation on thermal control surfaces / James R. Gaier and Stephen P. Berkebile.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo26337
  • Modeling of melt growth during carbothermal processing of lunar regolith / R. Balasubramaniam, S. Gokoglu, U. Hegde.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo27891
  • Computational study of the impact of unsteadiness on the aerodynamic performance of a variable-speed power turbine / Gerard E. Welch.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo27900
  • Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines / Daniel E. Paxson, Thomas A. Kaemming.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30483
  • Analysis of water extraction from lunar regolith / U. Hegde and R. Balasubramaniam, S. Gokoglu.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30532
  • Exhaust plume effects on sonic boom for a delta wing and a swept wing-body model / Raymond Castner, Troy Lake.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30596
  • Flow-field surveys for rectangular nozzles / K. B. M. Q. Zaman.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo28432
  • Active combustion control for aircraft gas-turbine engines : experimental results for an advanced, low-emissions combustor prototype / John C. DeLaat ... [and others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo31847
  • Research on supersonic inlet bleed / David O. David, Manan A. Vyas, and John W. Slater.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32068
  • Experimental study of boundary layer flow control using an array of ramp-shaped vortex generators / Stefanie M. Hirt, Khairul B.M.Q. Zaman, and Timothy J. Bencic.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32070
  • Design and analysis tool for external-compression supersonic inlets / John W. Slater.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32321
  • Progress toward accurate measurements of power consumptions of DBD plasma actuators / David E. Ashpis, Matthew C. Laun, Elmer L. Griebeler.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30421
  • Performance evaluation of a high bandwidth liquid fuel modulation valve for active combustion control / Joseph R. Saus [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo33032
  • Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing / Bryan Palaszewski.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo39373

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