@techreport{oai:jaxa.repo.nii.ac.jp:00002512,
 author = {弘松, 純 and 内海, 政春 and 島垣, 満 and 川崎, 聡 and 瀧田, 純也 and 中村, 智也 and Hiromatsu, Jun and Uchiumi, Masaharu and Shimagaki, Mitsuru and Kawasaki, Satoshi and Takida, Junya and Nakamura, Tomoya},
 month = {Oct},
 note = {A rocket turbopump, high-speed, high-power turbomachinery, has suffered from various rotor vibration problems up to the present time. Establishment of an integrated design method consisting of turbopump components is eagerly expected to suppress the rotor vibration. We are now studying the design method of optimal rotor system by using multidisciplinary optimization due to information-sharing of turbopump components (pump, bearing, seal and turbine). A quality function deployment (QFD) is employed to visualize of the relation between turbopump components., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0062042000, レポート番号: JAXA-RM-13-007},
 title = {QFD援用によるロケットターボポンプ多領域最適化設計},
 year = {2013}
}