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Zhiyun Wang

Nanjing University of Aeronautics and Astronautics

Yudao Street

210016

Nanjing,, 210016

China

  • Nanjing University of Aeronautics and Astronautics

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Experimental Study on the Effect of Pilot-/Main-Stage Axial Velocity Ratio on Ignition Performance in a Dual Annular Combustor

Number of pages: 28 Posted: 12 Sep 2025
Zhiyun Wang, Yaxin Shen, Yuanhao Deng, Wei Li and Yingwen Yan
Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics, affiliation not provided to SSRN, Nanjing University of Aeronautics and Astronautics and Nanjing University of Aeronautics and Astronautics
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Abstract:

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Dual Annular Combustor, Axial Velocity Ratio, Recirculation Zone, Ignition Boundary, Flame Kernel Propagation Modes