@article{oai:nagoya.repo.nii.ac.jp:00030699, author = {Sasoh, Akihiro and Chang, Xin-Yu and Murayama, Toshiyuki and Fujiwara, Toshi}, issue = {2}, journal = {Memoirs of the Faculty of Engineering, Nagoya University}, month = {Mar}, note = {The method of numerical calculation of three-dimensional radiative transfer from nonequilibrium air shock layers over a body is presented with some reviews on radiative transfer and molecular physics. A numerical technique, which reduces the necessitating memory size of a computational resource, thereby enabling one to conduct three-dimensional calculation, has been developed. This method is applied to radiative heat transfer problems under a reentry condition. The radiative structure of the hypersonic air shock layer generated around a body is closely related to the thermally nonequilibrium structure of the shock layer. A radiative heat transfer which is comparable with the convective one is calculated at such a high Mach number as 35 at an altitude 70 km. This result suggests the importance of radiative heat transfer in thermal design of a reentry vehicle.}, pages = {179--224}, title = {Three-dimensional calculation of radiative field in hypersonic air shock layers}, volume = {43}, year = {1992} }