Open AccessAnalysis of Boundary Layer in Solid Rocket Nozzle and Numerical Analysis of Thermal Response of Carbon/Phenolic using Finite Difference Method
Author(s) -
Sang Kyu Seo,
Hee Cheol Hahm,
Yoon Goo Kang
Publication year - 2018
Publication title -
journal of the korean society of propulsion engineers
Language(s) - English
Resource type - Journals
eISSN - 2288-4548
pISSN - 1226-6027
DOI - 10.6108/kspe.2018.22.1.036
Subject(s) - boundary layer , nozzle , rocket engine nozzle , solid fuel rocket , rocket (weapon) , carbon fibers , aerospace engineering , materials science , layer (electronics) , finite difference method , thermal analysis , thermal , numerical analysis , finite difference , mechanics , composite material , mathematics , physics , engineering , mathematical analysis , meteorology , propellant , composite number
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