Abstract
Actually, besides the missile, some complex surface such as the surface of missile, accessories and opening and closing mechanism for the missile bay etc. will have obvious influence on flow in the bay. In order to study the steady flow characteristics of the missile bay, the calculation model is established and simplified according to the research needs. The working condition is that a missile model is carried in the middle of the missile bay. The characteristics of the flow field in the bay at Mach 1.5 and Mach 3.5 are calculated and analysed under the above working condition.
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