Regenerative Cooling Channel Design of a Supersonic Combustor Considering High-Temperature Property of Fuel
نویسندگان
چکیده
منابع مشابه
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ژورنال
عنوان ژورنال: Journal of the Korean Society of Propulsion Engineers
سال: 2018
ISSN: 1226-6027,2288-4548
DOI: 10.6108/kspe.2018.22.6.037