Numerical simulations of temperature fields in the uncooled nozzle of a short-range anti-aircraft rocket engine with an insert in the critical section made of various materials
Abstract. The paper presents numerical simulations of transient heat conduction in the uncooled nozzle of a short-range anti-aircraft rocket engine. The calculations were made for the configuration of the nozzle with an insert in the critical section made of various materials. The inserts used were:...
محفوظ في:
| المؤلفون الرئيسيون: | , , , |
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| التنسيق: | Artigo |
| اللغة: | Inglês |
| منشور في: |
Military University of Technology, Warsaw
2021-03-01
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| سلاسل: | Biuletyn Wojskowej Akademii Technicznej |
| الموضوعات: | |
| الوصول للمادة أونلاين: | http://biuletynwat.pl/gicid/01.3001.0015.6955 |
| الوسوم: |
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