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http://dx.doi.org/10.6108/KSPE.2020.24.6.108

Feasibility Study of the Application of Infinite Tube Probe in High Temperature Environment  

Kim, Hyeonjun (Combustion Chamber Team, Korea Aerospace Research Institute)
Ryu, Chulsung (Combustion Chamber Team, Korea Aerospace Research Institute)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.24, no.6, 2020 , pp. 108-119 More about this Journal
Abstract
Dynamic pressure sensor used in liquid rocket engine combustor and gas turbine is recess-mounted usually because it should work in high temperature environment. Although recess-mounted method can protect it from combustion gas in high temperature, tube resonance occurs in a tube-cavity system. To reduce it, the infinite tube probe(ITP) was introduced in this study. The ITP model suggested in previous literature was validated with experimental data and frequency response characteristics were analyzed. Guidelines for designing the ITP were suggested as frequency response profiles varied with geometric information and physical properties using this model.
Keywords
Infinite Tube Probes; Natural Frequency; Pressure Transducer;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
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