@inproceedings{oai:jaxa.repo.nii.ac.jp:00039552,
 author = {Tani, Hiroumi and Teramoto, S. and Toki, T. and Yoshida, S. and Yamaguchi, K. and Okamoto, K.},
 month = {Jul},
 note = {5th European Conference for Aeronautics and Space Sciences, EUCASS 2013 (July 1-5, 2013.), Munich, Germany, "Many of liquid rocket engines used in first stage of launch vehicles operate at a pressure above the critical pressure of oxygen, 5.04 MPa. The cryogenic oxygen injected into a combustion chamber is heated up to several thousand kelvin, therefore the high-density cryogenic oxygen necessarily experiences sudden expansion called “pseudo-boiling”1 at the pseudo-critical temperature. The pseudo-boiling has large impact on the mixing characteristics, hence a jet injected from a temperature below the pseudo-critical temperature must be distinguished from that injected from a temperature above the pseudo-critical temperature. The former is referred to as “transcritical jet” while the latter is simply called supercritical jet. Quantitative measurement data of transcritical jets are indispensable both for the better understanding of mixing phenomena and for the validation of numerical methods, but there are only few quantitative experimental data made public.2 In this report, axial and radial temperature profiles of a single phase cryogenic nitrogen jet under supercritical pressure are measured, and the influence of pseudo-boiling upon the jet mixing will be discussed.", 資料番号: PA1510093000},
 publisher = {European Conference for Aeronautics and Space Sciences},
 title = {Temperature measurement of cryogenic nitrogen jets at supercritical pressure},
 year = {2013}
}