Supercritical Heat Transfer of Cryogenic-Propellant Methane in Rectangular Engine Cooling Channels

标题
Supercritical Heat Transfer of Cryogenic-Propellant Methane in Rectangular Engine Cooling Channels
作者
关键词
-
出版物
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER
Volume 26, Issue 2, Pages 313-321
出版商
American Institute of Aeronautics and Astronautics (AIAA)
发表日期
2012-04-13
DOI
10.2514/1.t3670

向作者/读者发起求助以获取更多资源

Find the ideal target journal for your manuscript

Explore over 38,000 international journals covering a vast array of academic fields.

Search

Ask a Question. Answer a Question.

Quickly pose questions to the entire community. Debate answers and get clarity on the most important issues facing researchers.

Get Started