並列タイトル等2連式バルブレスパルスバーナに関する研究-パルス燃焼の安定機構と混合様式-
タイトル（掲載誌）航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-955
一般注記Ensemble-averaged heat release rates and pressures inside the combustion chambers were measured to better understand the operating characteristics of a twin valveless pulse burner. The combustion flows were also visualized using a high-speed laser schlieren photography. A measurement system of OH chemiluminescence intensity and pressure transducers were used as diagnostic tools. Based on the well-known Rayleigh’s criterion, the effects on the combustion stabilities of varying the equivalence ratio and the mass flux are discussed. Results show that the phase difference between heat release rate and pressure contributes significantly to the pulse combustion stability. In addition, the phase difference does not depend on the mass flux but on the equivalence ratio, indicating that the fuel/air mixing is a determinant factor in the phase relationship. This mixing process was successfully visualized on the schlieren photographs.
資料番号: NALTR0955000
レポート番号: NAL TR-955
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45214&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ