@techreport{oai:jaxa.repo.nii.ac.jp:00043264,
 author = {高梨, 進 and 沢田, 恵介 and Takanashi, Susumu and Sawada, Keisuke},
 month = {Nov},
 note = {A numerical simulation of transonic flows over complete ASKA aircraft configuration is carried out. A computational grid system is constructed using the algebraic multi-block method. The Euler equations are numerically solved by the upwind finite volume scheme., 資料番号: NALSP0008011, レポート番号: NAL SP-8},
 title = {STOL機ASKAの空力シミュレーション},
 year = {1987}
}