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Effect of Cooling Channel Aspect Ratio on Rocket Thermal Behavior
Details
Effect of Cooling Channel Aspect Ratio on Rocket Thermal Behavior
Author(s)
Pizzarelli, Marco
Nasuti, Francesco
Onofri, Marcello
Date Issued
2014-07
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
URI
https://search.asi.it/handle/20.500.13025/7729
ISSN
0887-8722
Journal
Journal of Thermophysics and Heat Transfer