Supersonic combustion mode analysis of a cavity based scramjet

Y Meng, W Sun, H Gu, F Chen, R Zhou - Aerospace, 2022 - mdpi.com
Since flame stability is the key to the performance of scramjets, scramjet combustion mode
and instability characteristics were investigated by using the POD method based on a cavity …

Effect of fuel-injection distance and cavity rear-wall height on the flameholding characteristics in a Mach 2.52 supersonic flow

Z He, H Wang, F Li, Y Tian, M Wan, J Zhu - Aerospace, 2022 - mdpi.com
The ethylene-fueled flameholding characteristics of a cavity-based scramjet combustor are
experimentally and numerically investigated. The test facility used the air heater, which …

Experimental investigation of flameholding in scramjet combustor by pylon with plasma actuator based on Q-DC discharge

AA Firsov - Aerospace, 2023 - mdpi.com
This paper presents the results of testing and optimization of a plasma-assisted combustion
scheme based on a pylon for fuel injection equipped with a plasma actuator. Electrodes …

Three-Dimensional Compressible Chemically Reacting Computational Fluid Dynamics with Tensor Trains

S Demir, R Johnson, BT Bojko, AT Corrigan… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
This study assesses the accuracy and efficiency of a framework employing tensor trains to
represent flamelet progress variable manifolds in chemically reacting computational fluid …

Mechanisms of ignition and combustion instability in a scramjet combustor with micro-rocket torch using dynamic mode decomposition

S Ogawa - Physics of Fluids, 2024 - pubs.aip.org
Achieving ignition and stable combustion in scramjet combustors, which have residence
times of milliseconds, requires effective flame stabilization. Previous studies have explored …

Dynamic Mode Decomposition of the Combustion Flow Field in a Scramjet Combustor with a Cavity Flameholder

S Ogawa - AIAA AVIATION 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-3787. vid To clarify the forced
ignition instability and combustion instability by the micro-rocket torch using modal analysis …

Modal Analysis of Forced Ignition Characteristics using Micro-Rocket Torch in Supersonic Flow

S OGAWA - TRANSACTIONS OF THE JAPAN SOCIETY FOR …, 2024 - jstage.jst.go.jp
The forced ignition instability and combustion instability in a scramjet engine were
investigated experimentally and numerically using modal analysis. In this study, proper …

Effect of Ramp Height on Fuel-Air Mixing Characteristics for Dual Transverse Injection behind the Ramp in Supersonic Air Crossflow

M Zahedzadeh, F Ommi - Aerospace Mechanics, 2022 - maj.ihu.ac.ir
To improve the mixing of fuel and air in supersonic flows, various methods are used,
including the implementation of a ramp ahead of the injection port. In the present work, the …