@article{oai:jaxa.repo.nii.ac.jp:00033243,
 author = {土井原, 良次 and 西田, 迪雄 and Doihara, Ryouji and Nishida, Michio},
 journal = {The Institute of Space and Astronautical Science report. S.P. : Aerodynamics, Thermophysics, Thermal Protection, Flight System Analysis and Design of Asteroid Sample Return Capsule},
 month = {Mar},
 note = {Numerical studies of the shock layer of a super orbital reentry capsule have been conducted by using thermochemical nonequilibrium VSL (Viscous Shock Layer) equations. In the present analysis, vibrational temperature has been treated as individual molecular species vibrational temperature. The analysis has been performed for the MUSES-C reentry conditions, and the temperatures and chemical species mole fractions in the shock layer have been revealed for the typical reentry altitudes of 84 km and 64 km. Radiative heat flux and spectra have been also computed from the results of the VSL analysis to discuss the necessity of the multi vibrational temperature model. Finally, convective heat fluxes for the multi vibrational temperature model and three temperature model are compared., 資料番号: SA0200016000},
 pages = {83--91},
 title = {Viscous Shock Layer Studies of a Super Orbital Reentry Capsule Using a Multi Vibrational Temperature Model},
 volume = {17},
 year = {2003}
}