2014•한국추진공학회 학술대회논문집Requires access
분출 마하수에 따른 측추력기 주위 유동장 특성 연구
이윤우, 변영환, 이종국
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Abstract
An experimental study has been performed for investigation of the jet interaction in supersonic flow with supersonic wind tunnel MAF of Konkuk University. The experimental techniques include schlieren. Freestream Mach number 3 is designed to perform experiment and pressure ratio between freestream and side jet is 200. Side jet nozzle is designed 2 different injection mach number. The results showed that characteristic of each flow field.