Assessments of - Turbulence Model Based on Menter’s Modification to Rotta’s Two-Equation Model

Table 1

Unit test cases representing steady/unsteady, attached/separated, and wall/shear flows.

Case	Details and references	Flow characteristics
A.	2D zero pressure gradient flat plate [6] compared data from [6]	Attached/steady
B.	2D backward-facing step [6] compared with data from [7]	Separated/unsteady
C.	Flow over a hump model [8] compared with data from [8–10]	Separated/unsteady
D.	Axisymmetric subsonic jet [6] compared with experimental data from [11]	Steady/shear
E.	2D curved backward-facing step [6] will be compared with LES data from [12]	Separated/unsteady
F.	2D periodic hill [6] compared with LES data from [13]	Separated/unsteady
G.	2D NACA 4412 Airfoil trailing edge separation [6] compared with data from [14]	Separated/steady
H.	Stationary circular cylinder in cross flow with data from [15]	Wake/unsteady