Zobrazeno 1 - 10
of 29
pro vyhledávání: '"Woo Seok Seol"'
Publikováno v:
Journal of Thermal Science. 20:467-473
An integrated program was established to design a combustor for a liquid rocket engine and to analyze regenerative cooling results on a preliminary design level. Properties of burnt gas from a kerosene-LOx mixture in the combustor and rocket performa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f2550595805aafbf4c860b8ea5db07ef
https://doi.org/10.1007/s11630-011-0497-y
https://doi.org/10.1007/s11630-011-0497-y
Publikováno v:
Transactions of the Korean Society of Mechanical Engineers B. 34:817-824
An improved spray model of a pressure-swirl atomizer was developed and the grid dependency of the model was investigated. Since the Lagrangian-Eulerian approach was adopted for tracking droplets, very small grids could not be used. However, in order
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8306460ed0b60358e1a615e730e97b61
https://doi.org/10.3795/ksme-b.2010.34.9.817
https://doi.org/10.3795/ksme-b.2010.34.9.817
Publikováno v:
Transactions of the Korean Society of Mechanical Engineers B. 34:563-568
초록:30톤급액체산소/케로신액체로켓엔진개발의중간단계로터보펌프-가스발생기개회로연계시험이수행되었다.터보펌프-가스발생기개회로연계시험은엔진시스템작동모사환경시험으로서가
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6f85746f503f5255e8232e5e1072b0a8
https://doi.org/10.3795/ksme-b.2010.34.5.563
https://doi.org/10.3795/ksme-b.2010.34.5.563
Publikováno v:
Journal of Propulsion and Power. 23:131-139
Combustion stability boundaries are investigated experimentally using a subscale chamber for screening the split-triplet impinging jet injectors of a liquid propellant rocket engine. Geometrical dimensions and operating conditions of the subscale cha
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7310d8271b3ad46ecf5f1622a9a2f05a
https://doi.org/10.2514/1.19937
https://doi.org/10.2514/1.19937
Publikováno v:
Journal of Mechanical Science and Technology. 20:874-881
Combustion stability characteristics in actual full-scale combustion chamber of a rocket engine are investigated by experimental tests with the model (sub-scale) chamber. The present hot-fire tests adopt the combustion chamber with three configuratio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3c6073c55fb285973d330405d9730669
https://doi.org/10.1007/bf02915950
https://doi.org/10.1007/bf02915950
Publikováno v:
Journal of Mechanical Science and Technology. 19:1821-1832
This study realizes the conceptual method to predict combustion instability in actual full-scale combustion chamber of rocket engines by experimental tests with model (sub-scale) chamber. The model chamber was designed based on the methodologies prop
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::82c5364743db47b3c6344ef94d8a7cc0
https://doi.org/10.1007/bf02984194
https://doi.org/10.1007/bf02984194
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 33:64-70
The overall results of hot firing tests of fuel-rich gas generator with impinging injector at design and off-design points are described. The gas generator consists of an injector head with impinging injector, a water cooled combustor wall, a turbule
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0a999a0bcf4e34cdeb92de984362b3a5
https://doi.org/10.5139/jksas.2005.33.6.064
https://doi.org/10.5139/jksas.2005.33.6.064
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 33:69-77
To optimize and limit the axial length of the baffle of the KSR-III engine, stability rating tests using pulse gun as one of artificial disturbance devices have been done. Generally a rocket engine can be considered to be dynamically stable if a cert
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d64c771021453982d625ee3de4783278
https://doi.org/10.5139/jksas.2005.33.1.069
https://doi.org/10.5139/jksas.2005.33.1.069
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 32:102-111
The procedure of design and manufacture of sub-scale combustor using bipropellant swirl injector with external mixing for a liquid rocket engine are described. The results of cold flow test, ignition test and combustion test of the sub-scale combusto
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4ec254428d9859cabc1e3a0ad9a81564
https://doi.org/10.5139/jksas.2004.32.10.102
https://doi.org/10.5139/jksas.2004.32.10.102
Publikováno v:
Transactions of the Korean Society of Mechanical Engineers B. 28:945-952
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f56590272fc58a88753edce09e5da4d5
https://doi.org/10.3795/ksme-b.2004.28.8.945
https://doi.org/10.3795/ksme-b.2004.28.8.945