镁基水冲压发动机燃烧室长度及进水距离设计方法
Design Method of Combustion Chamber Length and Water Intake Distance of Magnesium-based Water Ramjets
Received date: 2010-04-23
Revised date: 2010-06-08
Online published: 2011-01-25
黄利亚 , 夏智勋 , 胡建新 , 韩超 , 朱千稳 , 周星 . 镁基水冲压发动机燃烧室长度及进水距离设计方法[J]. 航空学报, 2011 , 32(1) : 67 -74 . DOI: CNKI:11-1929/V.2010.1111.0911.017
Magnesium-based water ramjets with two water intakes are known for their better performances than those with only one intake. This article studies the design of the combustion chamber length and water intake distance on this type of water ramjets. Theoretical anlysis and experimental temperature data indicate that magnesium enters the combustion chamber as molten droplets, and the burning process of the droplets is controlled by vapor-phase diffusion. A simplified D3/2 law is used to calculate the droplet burning time. A method to design the combustion chamber length and water intake distance is developed on the basis of magnesium burning time and water evaporization time. The structure of a water ramjet prototype is improved with this method, and comparison tests are conducted for the two structures in a ground direct-connect testing system. An enhanced engine performance is obtained with the improved structure in the tests, which also testify the validity of the design method.
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