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Numerical Study on Combustor Flow-Path Design for a Scramjet Flight Experiment 高橋, 政浩 富岡, 定毅 小寺, 正敏 小林, 完 長谷川, 進 清水, 太郎 青野, 淳也 宗像, 利彦 TAKAHASHI, Masahiro TOMIOKA, Sadatake KODERA, Masatoshi KOBAYASHI, Kan HASEGAWA, Susumu SHIMIZU, Taro AONO, Junya MUNAKATA, Toshihiko ©2021 The Japan Society for Aeronautical and Space Sciences. Supersonic Combustion CFD Flight Experiment Ground Testing 形態: カラー図版あり Physical characteristics: Original contains color illustrations Accepted: 2020-06-15 資料番号: PA2110054000 日本航空宇宙学会(JSASS) Japan Society for Aeronautical and Space Sciences (JSASS) 2021 eng journal article VoR https://jaxa.repo.nii.ac.jp/records/48244 https://doi.org/10.2322/tastj.19.415 info:doi/10.2322/tastj.19.415 1884-0485 Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 19 3 415 423 https://jaxa.repo.nii.ac.jp/record/48244/files/PA2110054000.pdf application/pdf 2.3 MB 2022-01-11