Experimental Investigation on Aluminum-Based Water Ramjet for Propelling High-Speed Underwater Vehicles

IF 1.7 4区 工程技术 Q2 ENGINEERING, AEROSPACE Journal of Propulsion and Power Pub Date : 2023-08-08 DOI:10.2514/1.b39133
R. Murugesan, S. Chakravarthy, J. Kandasamy, R. Sarathi
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Abstract

Major challenges in developing and realizing a novel aluminum–water reaction-based water ramjet propulsion system for high-speed underwater vehicles and demonstration of a water-breathing jet propulsion test facility are investigated. Two stages of combustion, propellant grain combustion and subsequent water combustion, with primary combustion products are adopted. High-pressure-molded propellant grains up to 45% of micro–nano ([Formula: see text]) aluminum were prepared and combusted in the primary chamber, which exhibits mild ignition delay, and a residue of 4–6% was retained. Once water is injected into the secondary chamber, the net thrust generation is increased more than twice from the exhaust jet and improves the specific impulse by 40%. The lean fuel conditions in the secondary chamber lead to reduction in combustion propensity, which causes drop in [Formula: see text] efficiency. The ultrafine iron-oxide-catalyzed micro–nano blended propellants marginally improved the propulsive performance than the uncatalyzed compositions. The [Formula: see text] efficiency of the catalyzed propellants was enhanced up to 38.6%. Aluminum agglomeration in primary combustion considerably occurred; apparently, only a fraction of aluminum particles or agglomerates are completely burnt within the secondary chamber, and the remaining aluminum particles are either partially burnt or go unreacted.
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铝基水冲压发动机用于高速水下航行器的试验研究
研究了开发和实现用于高速水下航行器的新型铝-水反应水冲压发动机推进系统以及水呼吸式喷气发动机推进试验装置的主要挑战。燃烧分为两个阶段,推进剂颗粒燃烧和随后的水燃烧,燃烧产物为初级燃烧产物。制备了高达45%的微纳([公式:见正文])铝的高压成型推进剂颗粒,并在主室中燃烧,主室表现出轻微的点火延迟,并保留了4-6%的残留物。一旦将水注入二次室,排气射流产生的净推力增加了两倍以上,比冲提高了40%。副室中的贫燃料条件导致燃烧倾向降低,从而导致[公式:见正文]效率下降。超细氧化铁催化的微纳混合推进剂比未催化的推进剂略微提高了推进性能。催化推进剂的[公式:见正文]效率提高了38.6%。一次燃烧中出现了明显的铝团聚现象;显然,只有一小部分铝颗粒或团聚体在第二室中完全燃烧,其余的铝颗粒要么部分燃烧,要么未反应。
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来源期刊
Journal of Propulsion and Power
Journal of Propulsion and Power 工程技术-工程:宇航
CiteScore
4.20
自引率
21.10%
发文量
97
审稿时长
6.5 months
期刊介绍: This Journal is devoted to the advancement of the science and technology of aerospace propulsion and power through the dissemination of original archival papers contributing to advancements in airbreathing, electric, and advanced propulsion; solid and liquid rockets; fuels and propellants; power generation and conversion for aerospace vehicles; and the application of aerospace science and technology to terrestrial energy devices and systems. It is intended to provide readers of the Journal, with primary interests in propulsion and power, access to papers spanning the range from research through development to applications. Papers in these disciplines and the sciences of combustion, fluid mechanics, and solid mechanics as directly related to propulsion and power are solicited.
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