Paper Title
A Review on Experimental Work in Combustion Process of Scramjet Engine
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Registration ID: IJNRD_305400
Published ID: IJNRD2504271
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Keywords
Scramjet, Injection Strategy, Mach Number, Combustion Efficiency
Abstract
A Scramjet (Ramjet with Supersonic Combustion) also known as air-breathing jet engine which facilitates combustion at supersonic airflow velocities. The scramjet engine has numerous applications in military operations and space launches, with ongoing modifications aimed at enhancing its effectiveness. In this scramjet engine, combustion transpires at supersonic airflow, making the phenomenon of combustion crucial to understand in depth. This study provides an overview of several experimental studies conducted on the combustion processes of scramjet engines. The issue with Ramjets is that at elevated speeds (about Mach 6), the temperature of the input air approaches the exhaust temperature due to compression at the intake. Consequently, there will be a significant decline in the engine's efficiency and thrust. The velocity of ramjets cannot exceed Mach 6. To address numerous challenges, a new type of ramjet has been introduced, known as the scramjet engine. In a scramjet, all components are identical to those of a ramjet; however, the airflow remains supersonic throughout the compression process, meaning that the airflow within the entire engine is at supersonic velocity. This paper analyzes the characteristics of combustion within a scramjet combustor utilizing a modified flamelet model, presents an experimental assessment of the combustion performance of a dual-mode scramjet engine with kerosene as fuel, studies the process of incomplete combustion in a scramjet engine, along with the analysis of the characteristics of combustion of hydrogen and cracked kerosene in a DLR scramjet combustor employing a hybrid Reynolds-Averaged Navier-Stokes (RANS) and Large Eddy Simulation (LES) methodology, where the grid spacing are smaller than turbulent scales are resolved, It functions by resolving the larger turbulent scales while simulating the smaller scales, so greatly improving the comprehension of intricate flows that involve turbulence, compressibility, and combustion reactions; in addition to examining fuel injection, combustion efficiency, and the performance of scramjets with various fuels.
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How To Cite (APA)
Mafidur Rahman (April-2025). A Review on Experimental Work in Combustion Process of Scramjet Engine. INTERNATIONAL JOURNAL OF NOVEL RESEARCH AND DEVELOPMENT, 10(4), c402-c412. https://ijnrd.org/papers/IJNRD2504271.pdf
Issue
Volume 10 Issue 4, April-2025
Pages : c402-c412
Other Publication Details
Paper Reg. ID: IJNRD_305400
Published Paper Id: IJNRD2504271
Research Area: Science and Technology
Author Type: Indian Author
Country: -, -, India
Published Paper PDF: https://ijnrd.org/papers/IJNRD2504271.pdf
Published Paper URL: https://ijnrd.org/viewpaperforall?paper=IJNRD2504271
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