@inproceedings{oai:jaxa.repo.nii.ac.jp:00036737,
 author = {須浪, 徹治 and 徳永, 英紀 and 西岡, 通男 and Sunami, Tetsuji and Tokunaga, Hidenori and Nishioka, Michio},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Sep},
 note = {航空宇宙技術研究所 Sep. 1994 (15th). Mar. 1995 (16th) 東京 日本, National Aerospace Laboratory Sep. 1994 (15th). Mar. 1995 (16th) Tokyo Japan, 超音速流中の縦渦内の流れの諸量分布と、下流方向変化、縦渦列間の干渉・縦渦とジェットの干渉、縦渦内での乱流変化などを観察した。縦渦の初期配列が干渉の程度や、これによる乱流渦のスケールおよび混合の様子に大きく影響することが分かった。このことから、衝撃波・剪断層・縦渦の配置の操作により、超音速の流れ場および混合の制御、さらに燃焼・熱拡散の制御が自由にできると考えられる。複数のストラットによる縦渦列で、燃焼器内全域での混合を実現できる可能性がある。, Flow distributions in the streamwise vortices, change in downstream direction, interference between streamwise vortices, interference between streamwise vortex and jet stream, and change of turbulence in the streamwise vortex in the supersonic flow were observed. It was found that the degree of interferences and the scale of turbulence vortex and the change in mixing behavior derived from the interferences were strongly affected by the initial arrangement of streamwise vortices. From these results, it can be concluded that the supersonic flow field and mixing as well as the combustion and thermal diffusion can be freely controlled by the operation of the arrangement of shock wave, shear layer, and streamwise vortex. There is some possibilities of realizing the mixing in the whole region of combustor by the streamwise vortices with plural struts., 資料番号: AA0000109008, レポート番号: NAL SP-28},
 pages = {32--36},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {縦渦列を用いた超音速混合の制御},
 volume = {28},
 year = {1995}
}