高温来流下U型脉冲爆震燃烧室燃烧特性试验

Translated title of the contribution: Experiment on combustion characteristics of U⁃bend pulse detonation combustor under high temperature inlet stream

Wenhao Tan, Longxi Zheng, Jie Lu, Lingyi Wang, Kang Huang

Research output: Contribution to journalArticlepeer-review

5 Scopus citations

Abstract

In order to obtain the combustion characteristics of gas⁃liquid two⁃phase multi⁃cycle U⁃bend pulse detonation combustor (U⁃PDC) under high temperature inlet stream, experimental research was carried out by using gasoline and air as fuel and oxidant.The results indicated that the U⁃PDC can achieve stable operation at the working frequency of 15-38 Hz when the inlet temperature was 373 K, and the deflagration to detonation transition (DDT) distance was shortened when the working frequency increased.When the working frequency was 15-25 Hz, the detonation initiation failed at room temperature.The results showed that high temperature inflow can promote the DDT process.At room temperature and working frequency of 15-25 Hz, due to the uneven distribution of combustible gas in the U⁃bend detonation tube, the time when the flame was detected outside of the U⁃bend detonation tube was later than the exit of the U⁃bend detonation tube.When the inflow temperature increased to 373 K, the phenomenon was obviously improved.In addition, the ignition time of U‑PDC was within 3-10 ms, which was greatly affected by ignition delay time.When the working frequency of U⁃PDC was the same and the inlet stream temperature raised from room temperature to 373 K, the wave velocity increased, and the ignition time decreased.

Translated title of the contributionExperiment on combustion characteristics of U⁃bend pulse detonation combustor under high temperature inlet stream
Original languageChinese (Traditional)
Pages (from-to)502-510
Number of pages9
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume37
Issue number3
DOIs
StatePublished - Mar 2022

Fingerprint

Dive into the research topics of 'Experiment on combustion characteristics of U⁃bend pulse detonation combustor under high temperature inlet stream'. Together they form a unique fingerprint.

Cite this