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

Author:

Sarvankar Sumit S.1,Sarkar Drik2,Arasu Adrin Issai1,Mistry Chetankumar Sureshbhai3,Vadlamani Nagabhushana Rao1ORCID

Affiliation:

1. Department of Aerospace Engineering, Indian Institute of Technology Madras , Chennai, Tamil Nadu 600036, India

2. Department of Mechanical Engineering, Indian Institute of Technology Kharagpur , Kharagpur, West Bengal 721302, India

3. Department of Aerospace Engineering, Indian Institute of Technology Kharagpur , Kharagpur, West Bengal 721302, India

Abstract

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.

Publisher

ASME International

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