1–20 von 29 Ergebnissen
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    Ice Roughness and Thickness Evolution on a Business Jet Airfoil (AIAA 2018-3014)

    McClain, Stephen T. / Vargas, Mario M. / Tsao, Jen-Ching et al. | British Library Conference Proceedings | 2018

    Summary of Ice Shape Geometric Fidelity Studies on an Iced Swept Wing (AIAA 2018-3494)

    Woodard, Brian S. / Broeren, Andy P. / Lee, Sam et al. | British Library Conference Proceedings | 2018

    Independent Effects of Reynolds and Mach Numbers on the Aerodynamics of an Iced Swept Wing (AIAA 2018-3492)

    Broeren, Andy P. / Lee, Sam / Woodard, Brian et al. | British Library Conference Proceedings | 2018

    Comparison of Iced Aerodynamic Measurements on Swept Wing from Two Wind Tunnels (AIAA 2018-3493)

    Lee, Sam / Broeren, Andy P. / Woodard, Brian et al. | British Library Conference Proceedings | 2018

    Effect of Simulated Scalloped Ice on the Aerodynamics of a Swept-Wing at Low-Reynolds Number (AIAA 2018-3495)

    Sandhu, Navdeep / Soltani, Mohammad R. / Bragg, Michael B. et al. | British Library Conference Proceedings | 2018

    Ice Roughness and Thickness Evolution on a Business Jet Airfoil

    McClain, Stephen T. / Vargas, Mario M. / Tsao, Jen-Ching et al. | AIAA | 2018
    Verlag: The American Institute of Aeronautics and Astronautics

      Ice Roughness and Thickness Evolution on a Business Jet Airfoil

      McClain, Stephen T. / Vargas, Mario / Tsao, Jen-Ching et al. | NTRS | 2018
      Experiments were performed in the Icing Research Tunnel at NASA Glenn Research Center (GRC) to investigate the ice roughness and thickness ...
      Verlag: NASA National Aeronautics and Space Administration
      Schlagwörter: Air Transportation And Safety

    Independent Effects of Reynolds and Mach Numbers on the Aerodynamics of an Iced Swept Wing

    Broeren, Andy P. / Lee, Sam / Woodard, Brian et al. | AIAA | 2018
    Verlag: The American Institute of Aeronautics and Astronautics

    Summary of Ice Shape Geometric Fidelity Studies on an Iced Swept Wing

    Woodard, Brian S. / Broeren, Andy P. / Lee, Sam et al. | AIAA | 2018
    Verlag: The American Institute of Aeronautics and Astronautics

      Summary of Ice Shape Geometric Fidelity Studies on an Iced Swept Wing

      Woodard, Brian S. / Broeren, Andy P. / Lee, Sam et al. | NTRS | 2018
      were designed and manufactured for both an 8.9%-scale and 13.3%-scale semispan wing model of the CRM65 which has been established as the full ...
      Verlag: NASA National Aeronautics and Space Administration
      Schlagwörter: Air Transportation And Safety

    Comparison of Iced Aerodynamic Measurements on Swept Wing from Two Wind Tunnels

    Lee, Sam / Broeren, Andy P. / Woodard, Brian et al. | AIAA | 2018
    Verlag: The American Institute of Aeronautics and Astronautics

    Effect of Simulated Scalloped Ice on the Aerodynamics of a Swept-Wing at Low-Reynolds Number

    Sandhu, Navdeep / Soltani, Mohammad R. / Bragg, Michael B. et al. | AIAA | 2018
    Verlag: The American Institute of Aeronautics and Astronautics

      Effect of Simulated Scalloped Ice on the Aerodynamics of a Swept-Wing at Low-Reynolds Number

      Sandhu, Navdeep / Soltani, Mohamad Reza / Bragg, Michael B. et al. | NTRS | 2018
      This paper studied the aerodynamic effects of a single scalloped ice accretion and two lower fidelity ice-shape simulations. These data ...
      Verlag: NASA National Aeronautics and Space Administration
      Schlagwörter: Aircraft Design, Testing And Performance

    Implementation and Validation of 3-D Ice Accretion Measurement Methodology

    Lee, Sam / Broeren, Andy P. / Kreeger, Richard E. et al. | AIAA | 2014
    Verlag: The American Institute of Aeronautics and Astronautics

    Swept-Wing Ice Accretion Characterization and Aerodynamics

    Broeren, Andy P. / Potapczuk, Mark / Riley, James et al. | AIAA | 2013
    Verlag: The American Institute of Aeronautics and Astronautics

    Ice-Accretion Test Results for Three Large-Scale Swept-Wing Models in the NASA Icing Research Tunnel

    Broeren, Andy P. / Potapczuk, Mark G. / Lee, Sam et al. | AIAA | 2016
    Verlag: The American Institute of Aeronautics and Astronautics

    Effect of Ice Shape Fidelity on Swept Wing Aerodynamic Performance

    Camello, Stephanie / Bragg, Michael B. / Broeren, Andy P. et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

      Effect of Ice Shape Fidelity on Swept-Wing Aerodynamic Performance

      Camello, Stephanie C. / Bragg, Michael B. / Broeren, Andy P. et al. | NTRS | 2017
      . Simplified versions of an ice shape may help improve current ice accretion simulation methods and therefore aircraft design, certification, and ...
      Verlag: NASA National Aeronautics and Space Administration

    Low-Reynolds Number Aerodynamics of an 8.9% Scale Semispan Swept Wing for Assessment of Icing Effects

    Broeren, Andy P. / Woodard, Brian / Diebold, Jeffrey M. et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Convection from Hemispherical and Conical Model Ice Roughness Elements in Stagnation Region Flows

    Hughes, Michael T. / McClain, Stephen T. / Shannon, Timothy A. et al. | AIAA | 2016
    Verlag: The American Institute of Aeronautics and Astronautics

    Validation of 3-D Ice Accretion Measurement Methodology for Experimental Aerodynamic Simulation

    Broeren, Andy P. / Addy, Harold E. / Lee, Sam et al. | AIAA | 2014
    Verlag: The American Institute of Aeronautics and Astronautics

    Evaluation of Alternative Altitude Scaling Methods for Thermal Ice Protection System in NASA Icing Research Tunnel

    Lee, Sam / Addy, Harold E. / Broeren, Andy P. et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Aerodynamic Classification of Swept-Wing Ice Accretion

    Diebold, Jeffrey M. / Broeren, Andy P. / Bragg, Michael | AIAA | 2013
    Verlag: The American Institute of Aeronautics and Astronautics

    A Study of the Effects of Altitude on Thermal Ice Protection System Performance

    Addy, Harold E. / Oleskiw, Myron / Broeren, Andy P. et al. | AIAA | 2013
    Verlag: The American Institute of Aeronautics and Astronautics