• Login
    View Item 
    •   DSpace Home
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    •   DSpace Home
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Characteristics of Laminar Separation Bubble With Varying Leading-Edge Shapes and Deflections of the Trailing-Edge Flap

    Thumbnail
    View/Open
    gtp_146_10_101014.pdf (1.996Mb)
    Date
    2024
    Author
    Sarvankar, Sumit S.
    Sarkar, Drik
    Arasu, Adrin Issai
    Mistry, Chetankumar Sureshbhai
    Vadlamani, Nagabhushana Rao
    Metadata
    Show full item record
    Abstract
    A series of implicit large eddy simulations (ILES) is carried out to examine the characteristics of a leading edge (LE) separation bubble. The test case comprises a flat plate with an elliptic leading edge (ELE), which is equipped with a trailing edge flap. Simulations are carried out (a) at three different flap angles (20 deg, 30 deg, 90 deg) and (b) using two different geometries of ELE where the ratio of the semimajor to semiminor axis is set to either 2:1 or 4:1. The flap is modeled using the immersed boundary method, which is computationally economical as it avoids regenerating the grid for varying flap angles. The results show that (a) the flow separates at lower flap deflection angles with a decrease in the aspect ratio of the ELE from 4:1 to 2:1 (b) an increase in the flap angle promotes separation at the LE due to an increase in the blockage in the bottom passage and a subsequent increase in the flow incidence at the leading edge. Simulations are also carried out using the γ−Reθ transition model and comparisons are drawn against ILES and experiments. Although the qualitative trends predicted using both ILES and Reynolds-Averaged Navier–Stokes (RANS) agree with the experiments, both approaches predict relatively shorter separation bubbles. This is attributed to the excess flow blockage in experiments due to the support plates, which are not modeled in the simulations. Nevertheless, the results demonstrate the superior accuracy of ILES over the RANS model.
    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4302953
    Collections
    • Journal of Engineering for Gas Turbines and Power

    DSpace software copyright © 2002-2015  DuraSpace
    Contact Us | Send Feedback
    Theme by 
    @mire NV
     

     

    Browse

    All of DSpaceCommunities & CollectionsBy Issue DateAuthorsTitlesSubjectsThis CollectionBy Issue DateAuthorsTitlesSubjects

    My Account

    LoginRegister

    Statistics

    View Usage Statistics

    DSpace software copyright © 2002-2015  DuraSpace
    Contact Us | Send Feedback
    Theme by 
    @mire NV