@techreport{oai:jaxa.repo.nii.ac.jp:00043162,
 author = {黒崎, 隆二郎 and 片山, 雅之 and Kurosaki, Ryujirou and Katayama, Masayuki},
 month = {Nov},
 note = {This paper presents the Subsonic Computational Aerodynamic Program (SUSCAP) that we have developed as an effective design tool to reduce the cost and time of wind tunnel tests. This code is based on a potential flow Panel Method coupled with a vortex-sheets renewal technique. The main function of the code is aerodynamic coefficient estimation of a three dimensional flying object. Other functions are also added, that is, velocity estimation at arbitrary points apart from the boundary suface, and high subsonic flow simulation by Prandtl-Glauert transformation. In order to investigate the usefulness of the code in designing aerodynamic shapes, this code is applied to a Wing-Boby-Tail configuration and a cruciform missile configuration. Their pressure distributions and roll moments are calculated. Calculated results are compared with the measured data, and the agreement is found satisfactory., 資料番号: NALSP0003020, レポート番号: NAL SP-3},
 title = {パネル法による亜音速計算空カプログラムの開発},
 year = {1984}
}