20142018

Research output per year

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Research Output

  • 5 Conference contribution

An active variable camber continuous trailing edge flapped wing wind tunnel model for aeroelastic “in-flight” shape optimization tests

Precup, N., Mundt, T., Mor, M. & Livne, E., Jan 1 2018, 2018 Multidisciplinary Analysis and Optimization Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3106. (2018 Multidisciplinary Analysis and Optimization Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

  • 1 Scopus citations

    The design, construction, and tests of a concept aeroelastic wind tunnel model of a high-lift variable camber continuous trailing edge flap (HL-VCCTEF) wing configuration

    Precup, N., Mor, M. & Livne, E., Jan 1 2015, 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics Inc., (56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

  • Wind tunnel investigation of a flexible wing high-lift configuration with a variable camber continuous trailing edge flap design

    Nguyen, N. T., Precup, N., Livne, E., Urnes, J., Dickey, E., Nelson, C., Chiew, J., Rodriguez, D. L., Ting, E. & Lebofsky, S., Jan 1 2015, 33rd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, (33rd AIAA Applied Aerodynamics Conference).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

  • 11 Scopus citations

    Design, construction, and tests of an aeroelastic wind tunnel model of a variable camber continuous trailing edge flap (VCCTEF) concept wing

    Precup, N., Mor, M. & Livne, E., Jan 1 2014, 32nd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc., (32nd AIAA Applied Aerodynamics Conference).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

  • 11 Scopus citations

    Experimental investigation of a flexiblewing with a variable camber continuous trailing edge flap design

    Nguyen, N., Precup, N., Urnes, J., Nelson, C., Lebofsky, S., Ting, E. & Livne, E., Jan 1 2014, 32nd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc., (32nd AIAA Applied Aerodynamics Conference).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

  • 28 Scopus citations