• DocumentCode
    3292095
  • Title

    Research of Reynolds stress model in the aerodynamics of damping rings aircraft

  • Author

    Tang, Hong ; Chen, Guoguang ; Liu, Peng

  • Author_Institution
    Sch. of Mechatron. Eng., North Univ. of China, Taiyuan, China
  • fYear
    2011
  • fDate
    15-17 April 2011
  • Firstpage
    3486
  • Lastpage
    3489
  • Abstract
    Airflow disturbance affected aerodynamics of aircraft between damping rings. In order to simulate this disturbance, extra-fluent field of damping rings aircraft was analyzed by Reynolds stress model (LLR-QI) in this paper. Numerical simulations results indicate that spaces between damping rings affected drag coefficient, and keep to test results, to based on improving firing accuracy of the aircraft.
  • Keywords
    aerodynamics; aircraft; damping; drag; flow simulation; rings (structures); LLR-QI; Reynolds stress model; aerodynamics; airflow disturbance; damping ring aircraft; drag coefficient; firing accuracy; numerical simulations; Aerodynamics; Aircraft; Aircraft propulsion; Atmospheric modeling; Damping; Mechatronics; Stress; Reynolds stress model; aerodynamics; aircraft; damping ring; numerical simulation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electric Information and Control Engineering (ICEICE), 2011 International Conference on
  • Conference_Location
    Wuhan
  • Print_ISBN
    978-1-4244-8036-4
  • Type

    conf

  • DOI
    10.1109/ICEICE.2011.5778254
  • Filename
    5778254