@techreport{oai:jaxa.repo.nii.ac.jp:00043372,
 author = {サキャ, アンディ エカ and 中村, 佳朗 and 保原, 充 and Sakya, Andi E. and Nakamura, Yoshiaki and Yasuhara, Michiru},
 month = {Nov},
 note = {A typical transonic flow at M infinity =0.80 and Re=1 by 106 is numerically simulated by using the Yee-Harten TVD Scheme of Euler Backward Implicit method. This study treats unsteady, inviscid or viscous compressible flows. In the viscous flow case, two turbulence models are applied: Baldwin-Lomax model (BLM) and Stock-Haase model (SHM). Comparison with the experimental data shows a good agreement., 資料番号: NALSP0010043, レポート番号: NAL SP-10},
 title = {NACA0012翼まわりの遷音速流に関する予備研究},
 year = {1989}
}