An accurate RANS-based transition prediction approach (part II)

نویسندگان

چکیده

Abstract We present a CFD analysis of wind tunnel model the new laminar turbo-prop aircraft designed in frame European Clean Sky 2 programme. The work presents numerical results aerodynamic performance scaled innovative turboprop A/C wing by using approach that includes transition prediction. Numerical will be compared considering two different procedures: a) analyses which location is imposed and b) position evaluated. prediction flow extension based on framework coupling between high-fidelity RANS tool Linear Stability (LNS) solver. According to this method, boundary layer equations are written conical formulation solution onset obtained through an e N method LNS calculations.

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ژورنال

عنوان ژورنال: IOP Conference Series: Materials Science and Engineering

سال: 2022

ISSN: ['1757-8981', '1757-899X']

DOI: https://doi.org/10.1088/1757-899x/1226/1/012013