@techreport{oai:jaxa.repo.nii.ac.jp:00043181,
 author = {高橋, 大輔 and 桑原, 邦郎 and Takahashi, Daisuke and Kuwahara, Kunio},
 month = {Nov},
 note = {A finite difference method was developed to simulate aircraft icing. An air flow was calculated by solving compressible Navier-Stokes equations directly. The accretion of ice to the NACA0012 airfoil at various angles of attack was calculated from trajectries of supercooled liquid drops through that flow., 資料番号: NALSP0005001, レポート番号: NAL SP-5},
 title = {アイシングのシミュレーション},
 year = {1985}
}