@techreport{oai:jaxa.repo.nii.ac.jp:00044503,
 author = {西尾, 健二 and 能瀬, 弘幸 and 越沼, 威 and 井上, 重雄 and 臼井, 弘 and 大畑, 敏美 and NISHIO, Kenji and NOUSE, Hiroyuki and KOSHINUMA, Takeshi and INOUE, Shigeo and USUI, Hiroshi and OHATA, Toshimi},
 month = {Jan},
 note = {A temperature measuring apparatus for an atmospheric turbulence study which has been made by the Airframe Division and the Flight Research Division of the National Aerospace Laboratory was designed and examined. Ten sets of thermocouples used in a probe are connected in series, and an anti-electro noise amplifier is made which enables us to measure accurately the input signals from the probe installed on an aircraft. The probe has been calibrated in a wind tunnel under the conditions of the flow Mach number ranging from 0.1 to 0.3 and environmental tests in an air at various temperatures ranging from -30C to 30C have been made. Test results showed good characteristics and the apparatus was used for the atmospheric turbulence study. This report contains detailed dimensions of the apparatus and the characteristics obtained from the calibration tests., 資料番号: NALTR0260000, レポート番号: NAL TR-260},
 title = {気流全温度測定装置の試作},
 year = {1972}
}