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Fluent를 이용한 3톤급 액체로켓엔진 매니폴드 내 추진제 유동 균일성 해석
윤동호(Dongho Yun),조현택(Hyeontaek Jo),장현수(Hyeonsoo Jang),현성윤(Seongyoon Hyun),정진택(Jintaeg Jung),홍용기(Yonggi Hong),윤영빈(Yuongbin Yoon) 한국추진공학회 2023 한국추진공학회지 Vol.27 No.4
Flow analysis was performed using Fluent to determine flow uniformity of 3 tonf liquid rocket engine propellant manifold. Based on the manifold initial design, the shape of the fuel distribution plate and propellant pipe inlet was changed to improve flow uniformity, and the flow uniformity of the computational analysis results for these initial and modified designs was compared/analyzed. As a result of the computational analysis, it was confirmed that the flow uniformity of the revised design was improved compared to the initial design.
Fluent를 이용한 3톤급 액체로켓엔진 매니폴드 내 추진제 유동 균일성 해석
윤동호(Dongho Yun),조현택(Hyeontaek Jo),장현수(Hyeonsoo Jang),현성윤(Seongyoon Hyun),정진택(Jintaeg Jung),홍용기(Yonggi Hong),윤영빈(Yuongbin Yoon) 한국추진공학회 2023 한국추진공학회 학술대회논문집 Vol.2023 No.5
Flow analysis was performed using Fluent to determine flow uniformity of 3 tonf liquid rocket engine propellant manifold. Based on the manifold initial design, the shape of the fuel distribution plate and propellant pipe inlet was changed to improve flow uniformity, and the flow uniformity of the computational analysis results for these initial and modified designs was compared/analyzed. As a result of the computational analysis, it was confirmed that the flow uniformity of the revised design was improved compared to the initial design.