Cite
Impact of mixture mass flux on hydrodynamic blockage ratio and Mach number of rotating detonation combustor.
MLA
Noda, Tomoyuki, et al. “Impact of Mixture Mass Flux on Hydrodynamic Blockage Ratio and Mach Number of Rotating Detonation Combustor.” Acta Astronautica, vol. 207, June 2023, pp. 219–26. EBSCOhost, https://doi.org/10.1016/j.actaastro.2023.03.013.
APA
Noda, T., Matsuoka, K., Goto, K., Kawasaki, A., Watanabe, H., Itouyama, N., Kasahara, J., & Matsuo, A. (2023). Impact of mixture mass flux on hydrodynamic blockage ratio and Mach number of rotating detonation combustor. Acta Astronautica, 207, 219–226. https://doi.org/10.1016/j.actaastro.2023.03.013
Chicago
Noda, Tomoyuki, Ken Matsuoka, Keisuke Goto, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Jiro Kasahara, and Akiko Matsuo. 2023. “Impact of Mixture Mass Flux on Hydrodynamic Blockage Ratio and Mach Number of Rotating Detonation Combustor.” Acta Astronautica 207 (June): 219–26. doi:10.1016/j.actaastro.2023.03.013.