학술논문
Transient Analysis of Liquid Rocket Engine Chilldown and Startup by Conjugate Heat Transfer Approach
Document Type
Conference Paper
Author
Source
In: AIAA SciTech Forum and Exposition, 2024 , AIAA SciTech Forum and Exposition, 2024. (AIAA SciTech Forum and Exposition, 2024, 2024)
Subject
Language
English