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Journal: AerospaceVolume: 12Number: 68
Article: Numerical Investigation of the Effect of Equivalent Ratio on Detonation Characteristics and Performance of CH4/O2 Rotating Detonation Rocket Engine
  • Authors:
  • Xiao Xu1,
  • Qixiang Han1,* and
  • Yining Zhang2
Link: https://www.mdpi.com/2226-4310/12/1/68

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