Research Catalog

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  • HSCT4.0 application [microform] : software requirements specification / A.O. Salas ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS22851

  • Artificial neural networks applications [microform] : from aircraft design optimization to orbiting spacecraft on-board environment monitoring / Kenol Jules, Paul P. Lin.

    • 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/LPS51539

  • Fuel injector design optimization for an annular scramjet geometry [microform] / Christopher J. Steffen, Jr.

    • Text
    • [Cleveland, Ohio : NASA Glenn Research Center, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS56848

  • Optimization of designs for nanotube-based scanning probes [microform] / V.M. Harik, T.S. Gates.

    • Text
    • Hampton, VA : ICASE, NASA Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 2002]
    • 2002

  • Design, optimization, and evaluation of integrally-stiffened Al-2139 panel with curved stiffeners / David Havens ... [and others].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo22684

  • Basis function approximation of transonic aerodynamic influence coefficient matrix / Wesley W. Li and Chan-gi Pak.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24037

  • Deterministic design optimization of structures in OpenMDAO framework / Rula M. Coroneos and Shantaram S. Pai.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo27895

  • Design, optimization, and evaluation of A1-2139 compression panel with integral T-stiffeners / Sameer B. Mulani ... [and others].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo31180

  • Extension of an object-oriented optimization tool : use's reference manual / Chan-gi Pak and Samson S. Truong.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Armstrong Flight Research Center, March 2015.
    • 2015-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo59270

  • An automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization / Erik L. Axdahl.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2015.
    • 2015-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo62868

  • Utilizing direct numerical simulations of transition and turbulence in design optimization / Man M. Rai.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, December 2015.
    • 2015-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65165

  • Artificial neural networks applications : from aircraft design optimization to orbiting spacecraft on-board environment monitoring / Kenol Jules, Paul P. Lin.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2002.
    • 2002-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS51539

  • Fuel injector design optimization for an annular scramjet geometry / Christopher J. Steffen, Jr.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2003.
    • 2003-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS56848

  • Solution-space screening of a hypersonic endurance demonstrator / Bernd Chudoba [and four others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37147

  • Issues and strategies in solving multidisciplinary optimization problems / Surya Patnaik.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37985

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