Warimani, Mahammadsalman and Azami, Muhammad Hanafi and Alam, Noor and Khan, Sher Afghan and Patil, Suhas and Ramis, M. K. (2025) Comparative analysis of combustion performance using pure and blended hydrocarbon fuels in a pulse detonation engine. Journal of Engineering Physics and Thermophysics, 98 (5). pp. 1240-1251. ISSN 1062-0125 E-ISSN 1573-871X
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Abstract
A pulse detonation engine (PDE) is a supersonic propulsive device used in aerospace vehicles. PDE employs periodic detonations to provide power or propulsion. In the present work, the Zeldovich–von Neumann–Doring (ZND) model is used to assess PDE performance for pure hydrocarbon and hydrocarbon-blended fuels. The combustion flame temperature ratio, detonation velocity, pressure ratio, and performance parameters like specific thrust and specific impulse are analytically calculated for various fuels. The novelty of the present research is the fact that thermophysical and performance characteristics of hydrocarbon fuels and of their blends have approximately the same results as given in the NASA Chemical Equilibrium with Applications (NASA CEA) data. All of the parameters' values fall within the acceptable range of the NASA CEA described values. The hydrocarbon fuels such as propane, butane, kerosene, and methane are safe, clean-burning, nontoxic, and great energy sources, and They are used as alternative hydrocarbon fuels in PDE.
Item Type: | Article (Journal) |
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Uncontrolled Keywords: | analytical approach, hydrocarbon-blended fuel, pulse detonation engine, specifi c impulse, ZND model |
Subjects: | T Technology > TJ Mechanical engineering and machinery > TJ163.26 Energy conservation |
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button): | Kulliyyah of Engineering > Department of Mechanical Engineering Kulliyyah of Engineering |
Depositing User: | Prof. Dr. Sher Afghan Khan |
Date Deposited: | 09 Oct 2025 09:53 |
Last Modified: | 09 Oct 2025 09:53 |
URI: | http://irep.iium.edu.my/id/eprint/123569 |
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