Skip to main content
Fig. 7 | Advances in Aerodynamics

Fig. 7

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

Fig. 7

The components of the normalized total Reynolds stress \(\left\langle \tau _{12}^{RANS} \right\rangle /\left\langle \tau _w \right\rangle\) vs. the distance to the wall \(y_w\): a the resolved Reynolds stress \(-\left\langle \rho u^{\prime \prime }v^{\prime \prime } \right\rangle /\left\langle \tau _w \right\rangle\) and b the average of modeled SGS stress \(\left\langle \tau _{12}^{LES} \right\rangle /\left\langle \tau _w\right\rangle\)

Back to article page