@techreport{oai:jaxa.repo.nii.ac.jp:00006002,
 author = {新城, 淳史 and Shinjo, Junji},
 month = {Nov},
 note = {This paper briefly summarizes numerical simulations related to rocket combustion at Computational Science Research Group, Institute of Aerospace Technology. The first part describes the investigation of a supercritical hydrogen flame of rocket injector element. The flame and flame-holding structures are elucidated by this simulation. The second part examines the droplet breakup mechanism due to capillary force. The influence of ligament end is included for new modeling. These results will lead to combustor system simulation in the future., 資料番号: AA0049500018, レポート番号: JAXA-SP-06-006},
 title = {計算科学グループにおける燃焼計算},
 year = {2006}
}