Role of Jet Spacing and Strut Geometry on the formation of Large Scale Structures & Mixing Characteristics
arXiv:2101.11797 · doi:10.1063/1.5026375
Abstract
The present study primarily focuses on the effect of jet spacing and strut geometry on the evolution and structure of the large-scale vortices which play a key role in mixing characteristics in turbulent supersonic flows. Numerically simulated results corresponding to varying parameters such as strut geometry and jet spacing (Xn=nDj such that n=2, 3 & 5) for square jet of height Dj=0.6 mm is presented in the current study, while the work also investigates the presence of the local quasi-two-dimensionality for the X2(2Dj) jet spacing; however, the same is not true for higher jet spacing. Further, the tapered strut (TS) section is modified to the straight strut (SS) for investigation, where the remarkable difference in flow physics is unfolded between the two configurations for similar jet spacing (X2: 2Dj). The instantaneous density and vorticity contours reveal the structures of varying scales undergoing different evolution for the different configurations. The effect of local spanwise rollers is clearly manifested in the mixing efficiency and the jet spreading rate. SS configuration exhibits excellent near field mixing behavior amongst all the arrangements. However, in case of TS cases, only X2(2Dj) configuration performs better due to the presence of local spanwise rollers. The qualitative and quantitative analysis reveals that near-field mixing is strongly affected by the two-dimensional rollers, while the early onset of wake mode is another crucial parameter to have improved mixing. Modal decomposition performed for SS arrangement sheds light into the spatial and temporal coherence of the structures, where the most dominant structures are found to be the Von-Karman street vortices in the wake region.
References in corpus (2)
Cited by in corpus (9)
- Suppression of vortex shedding using a slit through the circular cylinder at low Reynolds number
- Role of corner flow separation in unsteady dynamics of hypersonic flow over a double wedge geometry
- Investigation of Shock Wave Interactions involving Stationary and Moving Wedges
- Characteristics of shock tube generated compressible vortex rings at very high shock Mach numbers
- Flow Characteristics of Elastically Mounted Slit Cylinder at Sub-critical Reynolds Number
- Effect of vortex and entropy sources in sound generation for compressible cavity flow
- Leading edge bluntness effects on the hypersonic flow over the double-wedge at multiple aft-wedge angles
- Investigation of injector-coupled combustion dynamics in a methane-oxygen combustor using large eddy simulation and dynamic mode decomposition
- Investigation of passive flow control over an airfoil using leading edge tubercles