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Fig. 9 | Advances in Aerodynamics

Fig. 9

From: Constrained large-eddy simulation of laminar-turbulent transition in compressible channel flows

Fig. 9

The components of the normalized total Reynolds stress \(\left\langle q_{2}^{RANS} \right\rangle /\left\langle q_w \right\rangle\) vary with the distance to the wall \(y_w\): a the resolved Reynolds stress \(-\left\langle \rho C_p v^{\prime \prime }T^{\prime \prime } \right\rangle /\left\langle q_w \right\rangle\) and b the average of modeled SGS stress \(\left\langle q_{12}^{LES} \right\rangle /\left\langle q_w\right\rangle\)

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