@inproceedings{oai:jaxa.repo.nii.ac.jp:00006598,
 author = {渡辺, 安 and 村上, 哲 and 藤原, 仁志 and Watanabe, Yasushi and Murakami, Akira and Fujiwara, Hitoshi},
 book = {宇宙航空研究開発機構特別資料: 第66回　風洞研究会議論文集, JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 66th Meeting},
 month = {Mar},
 note = {Supersonic wind tunnel test of the air intake for the jet-powered experimental airplane was conducted associated with the NAL SST project. In order to estimate the supercritical and subcritical operation margin, the short compact mass flow meter with high accuracy is required in the wind tunnel test. Such a compact mass flow meter was designed and applied to the wind tunnel test. However, the result of wind tunnel test indicates that there is some problems associated with the calibration of the mass flow meter to achieve high accuracy., 資料番号: AA0047428009, レポート番号: JAXA-SP-03-003},
 pages = {81--84},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {ジェット実験機インテークの超音速風洞試験},
 volume = {JAXA-SP-03-003},
 year = {2004}
}