@techreport{oai:jaxa.repo.nii.ac.jp:00044023,
 author = {高島, 一明 and 沢田, 秀夫 and 青木, 竹夫 and TAKASHIMA, Kazuaki and SAWADA, Hideo and AOKI, Takeo},
 month = {Aug},
 note = {A survey of the facilities for aerodynamic testing of airplane models at transonic speeds and high Reynolds numbers is presented.At first,the need for high Reynolds number transonic testing is reviewed,using some experimental results.Then,some new approaches to high Reynolds number testing,i.e.the cryogenic wind tunnel,the induction driven wind tunnel,the Ludwieg tube,the Evans clean tunnel and the hydraulic driven wind tunnel are described.Finally,this paper comments upon the level of development of high Reynolds number testing facilities in this country., 資料番号: NALTM0440000, レポート番号: NAL TM-440},
 title = {三次元レイノルズ数遷音速風胴の調査研究},
 year = {1981}
}