Author: Levin V.
Publisher: Springer Publishing Company
ISSN: 0010-5082
Source: Combustion, Explosion, and Shock Waves, Vol.46, Iss.4, 2010-07, pp. : 408-417
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Abstract
This paper discusses an approach to implementing the operation and designing the flow duct of a ramjet combustor. Methods of air compression, ignition, flame stabilization, and fuel combustion in the flow are considered for the purpose of implementing an effective process on a short length with moderate total pressure losses. Advantages of narrow-mode ramjet engines are noted. Comparative results of experiments on the burning of hydrocarbon fuels in the ramjet combustors are given.
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