Synchronous gliding arc plasma-assisted ignition characteristics within dual-cavity in a kerosene-fueled model scramjet combustorOA
Synchronous gliding arc plasma-assisted ignition characteristics within dual-cavity in a kerosene-fueled model scramjet combustor
Xing ZHENG;Zhibo ZHANG;Min JIA;Huifeng MIAO;Wei CUI;Yun WU
State Key Laboratory for Strength and Vibration of Mechanical Structures,School of Aerospace,Xi'an Jiaotong University,Xi'an 710049,China||Shaanxi Engineering Laboratory for Vibration Control of Aerospace Structures,School of Aerospace,Xi'an Jiaotong University,Xi'an 710049,China||National Key Lab of Aerospace Power System and Plasma Technology,Xi'an Jiaotong University,Xi'an 710049,ChinaNational Key Lab of Aerospace Power System and Plasma Technology,Xi'an Jiaotong University,Xi'an 710049,China||National Key Lab of Aerospace Power System and Plasma Technology,Air Force Engineering University,Xi'an 710038,ChinaNational Key Lab of Aerospace Power System and Plasma Technology,Air Force Engineering University,Xi'an 710038,ChinaNational Key Lab of Aerospace Power System and Plasma Technology,Air Force Engineering University,Xi'an 710038,ChinaNational Key Lab of Aerospace Power System and Plasma Technology,Air Force Engineering University,Xi'an 710038,ChinaNational Key Lab of Aerospace Power System and Plasma Technology,Xi'an Jiaotong University,Xi'an 710049,China||National Key Lab of Aerospace Power System and Plasma Technology,Air Force Engineering University,Xi'an 710038,China
Gliding arc plasma igniterPlasma assisted ignitionScramjetSupersonic combustionSynchronous ignition
Gliding arc plasma igniterPlasma assisted ignitionScramjetSupersonic combustionSynchronous ignition
《中国航空学报（英文版）》 2026 (6)
212-226,15
This study was co-supported by the National Natural Science Foundation of China(Nos.52488101,52025064 and 52376138),the Foundation Research Project of China(No.1002TJA22010)and the Fundamental Research Funds for the Central Universities,China(No.xzy022025069).
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