@inproceedings{oai:jaxa.repo.nii.ac.jp:00004005,
 author = {福成, 雅史 and 山口, 敏和 and 齋藤, 翔平 and 浅井, 健太 and 栗田, 哲志 and 小紫, 公也 and 小田, 靖久 and 梶原, 健 and 高橋, 幸司 and 坂本, 慶司 and Fukunari, Masafumi and Yamaguchi, Toshikazu and Saitoh, Shohei and Asai, Kenta and Kurita, Satoshi and Komurasaki, Kimiya and Oda, Yasuhisa and Kajiwara, Ken and Takahashi, Koji and Sakamoto, Keishi},
 book = {宇宙航空研究開発機構特別資料: 第45回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2013論文集, JAXA Special Publication},
 month = {Mar},
 note = {第45回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2013 (2013年7月4日-5日. タワーホール船堀), 東京, 45th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2013 (July 4-5, 2013. Tower Hall Funabori), Tokyo, Japan, The reed-valve air-breathing system was developed to improve air-breathing performance of the microwave rocket. Air-breathing performance test was conducted using a gyrotron. Pressure history in the thruster was measured and plateau pressure was evaluated. Air-flow through the reed valve was estimated by using CFD model assuming Bernoulli-Euler beam as the reed valve. As a result, normalized plateau pressure and normalized plateau time under multi-pulse operation were increased at all repetitive-pulse frequency up to 200 Hz., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0062268005, レポート番号: JAXA-SP-13-011},
 pages = {25--28},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {リード弁式吸気機構によるマイクロ波ロケットの推力性能改善},
 volume = {JAXA-SP-13-011},
 year = {2014}
}