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Combustion Instability Phenomena Observed During Cryogenic Hydrogen Injection Temperature Ramping Tests for Single Coaxial Injector Elements

Authors :
Yoshio Nunome
Takuo Onodera
Masaki Sasaki
Takeo Tomita
Kan Kobayashi
Yu Daimon
Source :
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Publication Year :
2011
Publisher :
American Institute of Aeronautics and Astronautics, 2011.

Abstract

For LOX/LH2 shear coaxial injectors, it is well-known that high-frequency combustion instabilities may occur when the injection temperature of hydrogen decreases below a certain value, but the mechanism of the initiation of combustion instability with a coaxial injector is still not clear. In the present study, firing tests were conducted with five types of single shear coaxial injector elements by using LOX and LH2 as propellants to further investigate the mechanism of the initiation of combustion instability during temperature-ramping changes during hydrogen injection. Results showed that unstable combustion was initiated when the hydrogen injection temperature decreased to less than a certain cryogenic temperature. The combustion instabilities observed in the present firing tests are discussed and classified into three different types.

Details

Database :
OpenAIRE
Journal :
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Accession number :
edsair.doi...........4615d9d10d75a7a0df9450ab6e8721ab
Full Text :
https://doi.org/10.2514/6.2011-6027