Transonic flow past the complex cavity-sub-cavity configurations
A. Kuniyil, H. Bansal, J. J. Patel, R. Kumar, R. Sriram, G. Kanagaraj, Niranjan S. Ghaisas, H. Ogawa, S. K. Karthick

TL;DR
This paper investigates unsteady transonic flow in complex cavity systems resembling scramjet engine integrations, analyzing flow physics, pressure oscillations, and passive control strategies using DES simulations.
Contribution
It introduces a detailed analysis of cavity-sub-cavity interactions in transonic regimes and evaluates passive control methods to reduce pressure oscillations.
Findings
High-pressure oscillations increase with Mach number.
Cavity topology significantly affects shear-layer dynamics.
Slotted sub-cavity effectively suppresses pressure loads.
Abstract
The study investigates the physics of unsteady flow in complex cavity geometries operating in the transonic regime. A two-dimensional Detached Eddy Simulation (DES) approach is used for the preliminary analysis. The cavity configuration examined in this work arises from the integration of a scramjet engine with a launch vehicle. In this integrated geometry, the isolator section serves as a deep sub-cavity, while the Single Expansion Ramp Nozzle (SERN) constitutes the primary cavity. The combined arrangement therefore constitutes a complex cavity-sub-cavity system, which is referred to as such throughout the paper. The qualitative analysis revealed a feedback loop within the complex cavity-sub-cavity system, leading to high-pressure oscillations across the geometry. A monotonic increase in pressure loading is observed with increasing Mach number. Varying the cavity topology demonstrated…
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