@techreport{oai:jaxa.repo.nii.ac.jp:00043861,
 author = {小野, 孝次 and 塚野, 雄吉 and ONO, Takatsugu and TSUKANO, Yukichi},
 month = {Jun},
 note = {Flight tests were conducted using a light airplane to investigate the effect of high lift devices upon stall speed.The “1-g-break Technique” was used for determining the stall speed.Test configurations were(1)modified configuration by incorporating slats as well as the boundary layer control on flaps and flaperons and(2)the same configuration less slats installation.The results were compared with the original configuration.For each test configuration,lift coefficients corresponding to the stall speeds obtained were plotted against flap setting angle with various test parameters such as power setting,suction capacity and flaperon droop angle.The flight test results were compared with wind turnel test data., 資料番号: NALTM0278000, レポート番号: NAL TM-278},
 title = {単発STOL実験機に関する研究: 失速特性試験},
 year = {1975}
}