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    High Fidelity Flowpath Analysis of a Supersonic Combustor Coupled to Innovative Inward-Turning Inlets

    Malo-Molina, Faure / Gaitonde, Datta / Ebrahimi, Houshang et al. | AIAA | 2009

    Reaction Dynamics and Probability Study of Aluminum-Viton-Acetone Droplets

    Datta, Sanjana / Pantoya, Michelle / Dikici, Birce et al. | AIAA | 2010

    Scramjet Combustor Analysis Integrated to an Innovative Inward Turning Inlet

    Malo-Molina, Faure / Gaitonde, Datta / Ebrahimi, Houshang et al. | AIAA | 2008

    Three-Dimensional Analysis of a Supersonic Combustor Coupled to Innovative Inward-Turning Inlets

    Malo-Molina, Faure J. / Gaitonde, Datta V. / Ebrahimi, Houshang B. et al. | AIAA | 2010

    Numerical Simulation of a Generic High-Speed Inlet/Combustor with Hydrocarbon Fuel

    Malo-Molina, Faure / Gaitonde, Datta / Ebrahimi, Houshang et al. | AIAA | 2006

    ROTOR BLADE TRANSPORTATION SYSTEM

    Freier Zugriff
    DATTA MADIREDDI VASU / JOHNSON STEPHEN BERTRAM / BALZANINI DE MACEDO VIEIRA JULIANA CRISTINA | Europäisches Patentamt | 2015

    Integrated Photonics for NASA Applications

    Krainak, Michael / Stephen, Mark / Bowers, John E. et al. | NTRS | 2019