@inproceedings{oai:jaxa.repo.nii.ac.jp:00014690,
 author = {大津, 広敬 and 宮澤, 政文 and Otsu, Hirotaka and Miyazawa, Masafumi},
 book = {宇宙航行の力学シンポジウム　平成14年度, Symposium on Flight Mechanics and Astrodynamics 2002},
 month = {Mar},
 note = {The two-temperature model was assessed for simulating the chemically and thermally nonequilibrium flows around the reentry vehicle. In this analysis, the effect of the parameters for the model on the thickness of the shock layer and the stagnation point heat flux are compared. The flow condition is that the reentry speed is 8.0 km/s at the altitude of 60 km. It was found that the effect of parameters on the thermal nonequilibrium inside the shock layer is significant. But the shock stand-off distance, shock shape, and the heat flux are not affected significantly., 資料番号: AA0045913003},
 pages = {9--12},
 publisher = {宇宙科学研究所, The Institute of Space and Astronautical Science (ISAS)},
 title = {再突入飛行環境のシミュレーションに用いられる2温度モデルの検証},
 year = {2003}
}