Acknowledgement
본 연구는 방산기술지원센터 주관의 국방무기 체계 핵심기술과제(응용연구)인 '고효율 소형 추력기 설계기술' 과제의 일환으로 수행되었습니다. 또한 KAIST에 ANSYS 라이센스를 제공해준 ANSYS Korea에 감사를 표합니다.
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