Ducts can be found in ventilation systems, cooling ducts and blade passages of turbines,centrifugal pumps and many other engineering installations. The properties of the flow inducts can significantly affect the performance and efficiency of these installation areas. Themajority of the flows in ducts and engineering applications are turbulent.The work presented in this thesis focuses on the analysis of turbulent flows inside squaresectioned ducts and ducts with bends. The accuracy of three different high resolution highorder schemes in the context of Implicit Large Eddy Simulation (ILES) is analysed. Theinfluence of a low Mach limiting technique, Low Mach Number Treatment (LMNT) is alsostudied. The schemes employed are Monotonic Upwind Scheme for Scalar ConservationLaws (MUSCL) with a 2nd order Monotonized Central (MC) and 5th order limiter, and a9th order Weighted Essential Non-Oscillatory (WENO) limiter.The first case studied is a duct of square cross section . In the absence of experimentaldata for the duct case, the data from a plain channel flow is used to shed light on the results.The flow analysis points out the generation of secondary motions created by the existence ofsurrounding walls. All schemes employed lead to a similarly developed turbulent flow thatis used to provide the turbulent boundary profile for the following case. LMNT proves tosignificantly assist MUSCL 2nd and 5th, that use it, in providing a turbulent profile similarto that of WENO 9th that did not employ the technique but is inherently less dissipative.The second case under study is that of a square sectioned duct with a 90o bend. Thesimulation output is in good agreement both qualitatively and quantitatively with the experimentaldata available in the literature. The generation of secondary flows inside the bendis observed without flow separation. Although the turbulent flow entering the domain isalmost the same for all cases, differences between the schemes are noticed especially afterthe middle of the bend. LMNT leads to an overprediction of turbulence after that area forboth schemes employing it while WENO 9th without LMNT provides the most accurateresults compared to those provided by the experiment.The results demonstrate applicability of ILES to strongly confined flows with secondarymotions and shed light on cognitive properties of a wide range of state of the art schemes.
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