Structural design and analysis of a Mach zero to five turbo-ramjet system
Structural design and analysis of a Mach zero to five turbo-ramjet system
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DOI：
10.2514/6.1993-1983
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发表时间：
1993-06
期刊：
影响因子：
--
通讯作者：
K. Spoth;P. Moses
中科院分区：
文献类型：
--
作者：
K. Spoth;P. Moses
本文讨论了马赫数为5乘波飞行器巡航飞行器的马赫数为0 ~ 5的涡轮冲压发动机推进系统的结构设计和分析。一个可靠的概念设计所需的分析细节的水平。发动机主要结构的有限元失效模式尺寸分析的结果。还讨论了发动机/机体一体化的重要性。
The paper discusses the structural design and analysis of a Mach zero to five turbo-ramjet propulsion system for a Mach five waverider-derived cruise vehicle. The level of analysis detail necessary for a credible conceptual design is shown. The results of a finite-element failure mode sizing analysis for the engine primary structure is presented. The importance of engine/airframe integration is also discussed.