Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Chul-Sung Ryu"'
Publikováno v:
Journal of the Korean Society of Propulsion Engineers. 25:19-27
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5ffe212b487f85d7452426c96928d18e
https://doi.org/10.6108/kspe.2021.25.4.019
https://doi.org/10.6108/kspe.2021.25.4.019
Publikováno v:
Journal of the Korean Society of Propulsion Engineers. 21:73-82
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5f329626e1101f62a502c4c70d8d0cb2
https://doi.org/10.6108/kspe.2017.21.6.073
https://doi.org/10.6108/kspe.2017.21.6.073
Publikováno v:
Journal of the Korean Society of Propulsion Engineers. 19:64-71
Spinning process is generally used for manufacturing axisymme trical, thin-walled thickness and hollow circular cross-section parts. Traditional spinning techn ology is classified to conventional spinning and power spinning(shear spinning and flow fo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::746f32058309de298d8897b4aa1a065e
https://doi.org/10.6108/kspe.2015.19.6.064
https://doi.org/10.6108/kspe.2015.19.6.064
Publikováno v:
Journal of the Korean Society of Propulsion Engineers. 18:88-95
Spinning process to inner wall has been applied for reducing the weight of regenerative cooling chamber of liquid propellent rocket engine. The fractures of th e blanks of cylinder part and nozzle throat part have been observed during spinning proces
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::52044629a8a5610aa26246ed8c6ceb50
https://doi.org/10.6108/kspe.2014.18.6.088
https://doi.org/10.6108/kspe.2014.18.6.088
Publikováno v:
Journal of the Korean Society of Propulsion Engineers. 17:103-115
․ Chul-Sung Ryu** ․ Byoung-Jik Lim* ․ Hwan-Seok Choi*ABSTRACT Durability testing method trends of the thermal barrier coati ng(TBC) for the combustion chamber of the liquid-propellant rocket engine have been investigated. Many types of the dura
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eb0f3f337d2755529fe8ff1ceb037cf8
https://doi.org/10.6108/kspe.2013.17.1.103
https://doi.org/10.6108/kspe.2013.17.1.103
Publikováno v:
Journal of the Korean Society of Propulsion Engineers. 16:97-103
The combustion chamber and nozzle of a liquid rocket engine should be protected from the high temperature combustion gas generated by the chamber. An upper-stage nozzle extension has a large expansion ratio, therefore, The light-weight refractory mat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::25974db706306572eca3799b56103f07
https://doi.org/10.6108/kspe.2012.16.3.097
https://doi.org/10.6108/kspe.2012.16.3.097
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 37:1201-1208
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Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7e9c649d87f8190ff926a259207160fd
https://doi.org/10.5139/jksas.2009.37.12.1201
https://doi.org/10.5139/jksas.2009.37.12.1201
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 37:1096-1103
The predictions of the material behavior for the structural stability of thrust chamber mixing head at very-low temperatures are very important since the head is highly pressurized by the liquid oxygen with very-low temperatures and experiences impac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f7fa3ef0732122a078af76b123821717
https://doi.org/10.5139/jksas.2009.37.11.1096
https://doi.org/10.5139/jksas.2009.37.11.1096
Publikováno v:
Journal of the Korean Society for Aeronautical Space Science. 37:939-945
The dome stretching tests and tension tests have been performed to obtain a forming limit curve(FLC) for the copper alloy which is used for manufacturing the regenerative cooling thrust chamber. For experimental investigation of the forming limit cur
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9d65243cc0c8e61ad169756e5aed7e06
https://doi.org/10.5139/jksas.2009.37.9.939
https://doi.org/10.5139/jksas.2009.37.9.939
Autor:
Hwan-Seok Choi, Chul-Sung Ryu
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 36:271-278
A study has been conducted on the bulging process of liquid rocket engine nozzle which is essential to the manufacturing regenerative cooling combustion chamber. Mechanical properties of the material used for the bulging were experimentally obtained
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::90fde22acc7b2a741fc54b486dfeb7ad
https://doi.org/10.5139/jksas.2008.36.3.271
https://doi.org/10.5139/jksas.2008.36.3.271