@techreport{oai:jaxa.repo.nii.ac.jp:00043524,
 author = {サキャ, アンデイ エカ and 中村, 佳朗 and 保原, 充 and Sakya, Andi Eka and Nakamura, Yoshiaki and Yasuhara, Michiru},
 month = {Dec},
 note = {Two turbulence models have been used to simulate a typical flow around NACA-0012 at zero angle of attack. Those turbulence models are the Cebeci-Smith Model (CSM) and the Baldwin-Lomax Model (BLM). Analysis of these models in terms of turbulent boundary layer has also been carried out in which the differences in the predicted turbulent characteristics are made clear. The computed result is compared with the experimental data obtained from the transonic tunnel at Nagoya University., 資料番号: NALSP0016028, レポート番号: NAL SP-16},
 title = {Transonic Flow Calculation around NACA-0012},
 year = {1991}
}