• DocumentCode
    3205169
  • Title

    Aerodynamics characteristic of UiTM´s BWB UAV Baseline-II at different canard deflection angles at low pitching angle

  • Author

    Reduan, Nor Fazira ; Wisnoe, Wirachman ; Kuntjoro, Wahyu ; Nasir, Rizal Effendy Mohd ; Mohamad, Firdaus ; Ali, Zurriati

  • Author_Institution
    Faculty of Mechanical Engineering, Universiti Teknologi Mara, 40450 Shah Alam, Malaysia
  • fYear
    2010
  • fDate
    5-7 Dec. 2010
  • Firstpage
    1005
  • Lastpage
    1009
  • Abstract
    This paper discusses the influence of canard deflection angle on the aerodynamics characteristic of a Blended Wing Body (BWB) Baseline-II aircraft obtained from wind tunnel test. Canard is added as longitudinal control. All tests are carried out in UiTM Low Speed Wind Tunnel using 1/6 scaled model at around 0.1 Mach number at several canard angle. The result of the lift coefficient (CL), the drag coefficient (CD), and the pitching moment coefficient (CM), are plotted and analyze to show the characteristics of the BWB with different canard deflection angles.
  • Keywords
    Aerodynamics; Aircraft; Aircraft propulsion; Computational fluid dynamics; Elevators; Military aircraft; Unmanned aerial vehicles; Aerodynamics; Blended Wing Body; Unmanned Aerial Vehicles; Wind Tunnel;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Science and Social Research (CSSR), 2010 International Conference on
  • Conference_Location
    Kuala Lumpur, Malaysia
  • Print_ISBN
    978-1-4244-8987-9
  • Type

    conf

  • DOI
    10.1109/CSSR.2010.5773677
  • Filename
    5773677
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3205169