2026-03-14T22:48:16Z https://jaxa.repo.nii.ac.jp/oai

oai:jaxa.repo.nii.ac.jp:00022940 2023-06-20T19:37:15Z 1887:1888

Effects of Relative Spatial Arrangement between Swirl Vanes and Fuel Injection Holes for Main Nozzle on Fuel Distributions and Emission Characteristics of a Lean -Staged Burner for an Aero-Engine 航空用希薄ステージバーナの燃料分布及び排出ガス特性に及ぼすメインノズル旋回翼と燃料噴射孔の周方向位置関係の影響 上坂, 俊也 江口, 貴広 松浦, 一哲 山本, 武 林, 茂 Uesaka, Shunya Eguchi, Takahiro Matsuura, Kazuaki Yamamoto, Takeshi Hayashi, Shigeru NOx emissions Aero-engine combustor Optical burner/injector Staged lean-burn injector Laser induced fluorescence Optical refraction correction 形態: 図版あり Physical characteristics: Original contains illustrations 資料番号: PA1820010000 journal article 日本ガスタービン学会(GTSJ) Gas Turbine Society of Japan (GTSJ) 2018-03 日本ガスタービン学会誌 2 46 153(71) 161(79) Journal of the Gas Turbine Society of Japan 0387-4168 AN00186926 https://jaxa.repo.nii.ac.jp/records/22940 jpn (c)2018 公益社団法人日本ガスタービン学会 http://www.gtsj.org/method/copyright.html | http://www.gtsj.org/method/copyright.html metadata only access