@article{oai:jaxa.repo.nii.ac.jp:00031469,
 author = {浅沼, 強 and 田中, 英穂 and 谷田, 好通 and ASANUMA, Tsuyoshi and TANAKA, Hideo and TANIDA, Yoshimichi},
 issue = {4_B},
 journal = {東京大学宇宙航空研究所報告},
 month = {Dec},
 note = {A small wind-tunnel has been prepared for the calibration of some probes, which are used for the measurement of high-speed flow in turbomachines.Its specifications are as follows. Diameter of convergent nozzle: 50mm, 75mm. Maximum Mach number: 1 Back pressure: variable (1～3ata), 資料番号: SA0124355000},
 pages = {432--437},
 title = {<論文>検定風洞(高速内部流体実験施設報告)},
 volume = {1},
 year = {1965}
}