Effect of large-scale vortical structure on mixing and spreading of shear layer is numerically investigated. Two strut configurations namely Straight & Tapered strut at two convective Mach numbers (Mc = 1.4 & 0.37) for two jet heights (0.6 & 1mm) are investigated. Hydrogen jet is injected through a two-dimensional slot in oncoming coflow at Mach 2. Excellent agreement between simulated and experimental data is witnessed, whereas the instantaneous data reveal the presence of various large-scale structures in the flow field. From the instantaneous field, it becomes apparent that both the geometries have different vortical breakdown locations. It is also noticed that an early onset of vortex breakdown manifests itself into the mixing layer thickness enhancement, effect of which is reflected in overall mixing characteristics. It becomes evident that the shear strength plays an important role in the near field mixing. The higher shear strength promotes the generation of large vortices. The analysis shows that SS-0.6 case offers highest mixing efficiency being dominated by relatively large-scale structures. Eigenmodes obtained through Proper Orthogonal Decomposition (POD) confirm the presence of dominating structures and shed light into the series of events involved in vortex pairing/merging and breakdown. Dynamic modal decomposition (DMD) also strengthens the observation made through the POD.
I. INTRODUCTIONThe very notion of atmospheric flight at hypervelocity regime may appear fascinating and appealing but there are certain intrinsic challenges that need to be addressed. The concept of Scramjet was conceived as an air-breathing propulsion system, which is capable of propelling in high Mach number regime. But before the concept is realized certain questions need to be answered related to the design and technological issues. Although the proposed design may appear simple but achieving a stable and sustainable combustion efficiently at these speeds is an engineering marvel. The recent interest in Scramjet has promoted research towards the understanding of supersonic mixing phenomenon. The residence time being exceptionally short and need for efficient combustor has motivated research community to explore the underlying physics governing the mixing in these flow regimes.Various injector configurations have been explored and studied, most popular being normal, oblique and parallel each of them is having their own pros and cons, while the detailed discussion can be found in [1][2][3] . Due to the simplicity of the ____________________________