The impact of film cooling on the heat release within a rotating detonation combustor

Shreyas Ramanagar Sridhara , Antonio Andreini , Marc D. Polanka , Myles D. Bohon
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Abstract

Rotating detonation combustors establish a detonation wave that continuously circulates inside a small annulus. The presence of the detonation wave and the downstream oblique shock within the small annulus coupled with high mass flow induces a high heat load to the combustor wall. Preliminary analysis shows that for higher thermal power, internal air cooling alone is not sufficient to remove the heat out of the walls to maintain them below the maximum temperature of the metal. A possible solution is to use film cooling to reduce the heat flux to the combustor walls. One issue, though, is that the introduction of film cooling provides additional air into the system that can influence the combustion process as well as providing a location for secondary combustion.
This paper represents the first investigation to study the secondary implications on combustion of using film cooling in a rotating detonation combustor. The TU Berlin RDC architecture was modified with the introduction of 480 film cooling holes placed in the oblique shock region. High fidelity LES investigations were performed for different coolant plenum pressures to show the benefits of using film cooling. However, due to the presence of unburnt fuel in this post-detonation region, the coolant can result in additional combustion leading to an increase in temperature near the wall. One the one hand, these secondary reactions result in an increase of the overall heat release increasing combustion efficiency, however this also results in higher temperatures and reduced film cooling effectiveness. A simulation performed with nitrogen as a coolant enabled the effects of increased mixing caused by the ejection of coolant gases to be separated from the additional heat release. The simulation with nitrogen shows a reduction of 88% in the local heat release in the post detonation region resulting in similar performance as the uncooled case and significantly cooler walls.
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薄膜冷却对旋转爆燃燃烧器内热量释放的影响
旋转爆燃燃烧器产生的爆燃波在一个小环形空间内不断循环。在小环形空间内存在的爆轰波和下游斜冲击,加上高质流量,给燃烧器壁带来了高热负荷。初步分析表明,对于较高的热功率,仅靠内部空气冷却不足以将热量排出壁外,使其保持在金属最高温度以下。一种可能的解决方案是使用薄膜冷却来降低燃烧器壁的热通量。本文是首次研究在旋转爆燃燃烧器中使用薄膜冷却对燃烧的二次影响。对柏林工业大学的 RDC 结构进行了修改,在斜冲击区域引入了 480 个薄膜冷却孔。针对不同的冷却剂柱面压力进行了高保真 LES 研究,以显示使用薄膜冷却的好处。然而,由于未燃烧的燃料存在于这一爆燃后区域,冷却剂可能会导致额外的燃烧,从而导致壁附近的温度升高。一方面,这些二次反应会增加整体放热量,提高燃烧效率,但同时也会导致温度升高,降低薄膜冷却效果。使用氮气作为冷却剂进行模拟,可以将冷却剂气体喷出造成的混合增加与额外热量释放的影响区分开来。使用氮气进行的模拟显示,爆燃后区域的局部热量释放减少了 88%,因此性能与未冷却的情况类似,但壁面温度明显降低。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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