@techreport{oai:jaxa.repo.nii.ac.jp:00043441,
 author = {古浦, 勝久 and 金松, 恵美 and 高平, 幹成 and Koura, Katsuhisa and Kanematsu, Emi and Takahira, Mikinari},
 month = {Nov},
 note = {The "rarefied gas numerical wind tunnel" constructed on the National Aerospace Laboratory Numerical Simulator System with the universal code described using the null-collision direct-simulation Monte Carlo method is used for the simulation of rarefied gas flows around a flat-plate delta wing at a large angle of attack. Some flowfield properties shown by computer graphics are presented., 資料番号: NALSP0014008, レポート番号: NAL SP-14},
 title = {希薄気体数値風洞 VI. デルタ翼},
 year = {1990}
}