Experimental Investigation on Two-Phase Rotating Detonation Fueled by Kerosene in a Hollow Directed Combustor
نویسندگان
چکیده
The operating characteristic of two-phase rotating detonation fueled by kerosene in a hollow combustor with the isolation section is experimentally studied. When air mass flow rate 1.5 kg/s, equivalence ratio 0.98, and total temperature mixture 650 K, stable wave (RDW) obtained, which verifies feasibility designed (RDC). It found that there high-frequency oblique shock induced upstream section. A series experimental tests have been carried out changing incoming , an important factor affecting initiation. equivalent reactants between 0.950–1.152, single-wave formed. With increase ratio, time establishment decreases, intensity frequency increases, engine tail flame rises. chamber pressure Δp φ was defined, curve performance RDC obtained. velocity RDW increases has optimal value, higher or lower will lead to decrease combustion performance.
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ژورنال
عنوان ژورنال: Frontiers in Energy Research
سال: 2022
ISSN: ['2296-598X']
DOI: https://doi.org/10.3389/fenrg.2022.951177