Combustion Characteristics in Rotating Detonation Engines

نویسندگان

چکیده

A lot of studies on rotating detonation engines have been carried out due to the higher thermal efficiency. However, number, directions, and intensities waves are changeful when flow rate, equivalence ratio, inflow conditions, engine schemes vary. The present experimental results showed that combustion mode a was influenced by combustor scheme. annular channel had an outer diameter 100 mm inner 80 mm. Air hydrogen were injected into from 60 cylindrical orifices in 2 circular with width mm, respectively. When air mass rate increased keeping constant, varied. Deflagration diffusive combustion, multiple counterrotating waves, longitudinal pulsed detonation, single wave occurred. Both occurred at different times same operation. They could change between each other, evolution direction depended rate. operations ratios lower than 0.60, which helpful for cooling infrared stealth. generation mechanism is developed.

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ژورنال

عنوان ژورنال: International Journal of Aerospace Engineering

سال: 2021

ISSN: ['1687-5966', '1687-5974']

DOI: https://doi.org/10.1155/2021/8839967