Aerodynamic Prediction of High-Lift Configuration Using k?v2¯?? Turbulence Model

نویسندگان

چکیده

The aerodynamic performance of the high-lift configuration greatly influences safety and economy commercial aircraft. Accurately predicting configuration, especially stall behavior, is important for aircraft design. However, complex flow phenomena configurations pose substantial difficulties to current turbulence models. In this paper, a three-equation k-(v^2)-{\omega} model Reynolds-averaged Navier-Stokes equations used compute behavior configurations. A separated shear layer fixed function implemented in better capture nonequilibrium characteristics turbulence. Different configurations, including two-dimensional multielement NLR7301 Omar airfoils full-configuration (JAXA Standard Model), are numerically tested. results indicate that effect significant free layer, which key accurately devices. modified SPF k-(v^2 )-{\omega} more accurate than Spalart-Allmaras, stress transport, original models full configuration. relative errors predicted maximum lift coefficients within 3% experimental data.

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ژورنال

عنوان ژورنال: AIAA Journal

سال: 2021

ISSN: ['0001-1452', '1533-385X', '1081-0102']

DOI: https://doi.org/10.2514/1.j060939