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NTIS 바로가기한국정밀공학회지 = Journal of the Korean Society for Precision Engineering, v.34 no.11, 2017년, pp.789 - 795
이동균 (LIG넥스원 기계연구소) , 김준수 (LIG넥스원 기계연구소) , 박성우 (LIG넥스원 기계연구소) , 강성욱 (LIG넥스원 기계연구소)
In this study, a numerical analysis for predicting the internal pressure of the flight vehicle system with relief valve and N2-injection type cooler was conducted to operate the system safely in an unsteady-state condition. By adopting an incompressible ideal gas equation to computational domain at ...
NASA Space Vehicle Design Criteria (Structure), “Compartment Venting,” NASA SP-8060, 1970.
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IBS Inc., http://www.ask-ibs.jp/english (Accessed 19 OCT 2017)
MIL-STD-810G, http://everyspec.com/MIL-STD/MIL-STD-0800-0899/MIL-STD-810G_12306/ (Accessed 19 OCT 2017)
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