열음향 공진에 대한 초기실험결과

An ignitor for the initiation of burning propellants becomes one of the most critical components for the operation of liquid rocket engines. The main objective of the present study is to acquire an advanced technology for the sound and repeatable ignition source by use of the thermoacoustic resonance phenomenon. This paper mainly includes experimental results on heat generation from the thermoacostic resonance phenomenon and the ultimate goal is to develop an ignitor capable of multiple ignitions based on research results about the usage of the thermoacoustic resonance phenomenon.