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E. B. Brewer and C. E. Craven,"Experimental Investigation of Base Flow Field at High Altitude for a Four-Engine Clustered Nozzle Configuration", NASA-TND-5164, 1969
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R. A. Wasco and T. L. Cover, "Experimental Investigation of Base Flow Field at High Altutude for Configuration of Four and Five Clustered Nozzle", NASA TM X-1371, 1967
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R. J. Sergeant, " Base Heating Scaling Criteria for a Four Engine Rocket Cluster Operating at High Altitude", AIAA Paper 65-826
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T.-S. Wang, "Grid Resolved Analysis of Base flowfiled for four engine clustered nozzle configuration", J. of Spacecraft and Rocket, Vol. 33, No. 1, 1996
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T.-S. Wang, "Numerical Analysis of Base Flowfield for a Four Engine Clustered Nozzle Configuration," J. of Propulsion and Power, vol.11, No.5,
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R. Nallasamy et al, "Numerical Simulation of the Base Flow and Heat Transfer characteristics of a Four Nozzle Clustered Rocket Engine", AIAA 2008-4128
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F. Nasuti, etc, "Three Dimensional Features of Clustered Plug Flow", AIAA 2003-4910,
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B. H. Goethert, "Base Flow Characteristics of Missiles With Cluster-Rocket Exhausts", Aerospace Engieering, March 1961.
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9 |
N. T. Musial and J. J. Ward, "Base Flow Characteristics for Several Four Clustered Rocket Configurations at Mach Numbers from 2.0 to 3.5", NASA TN D-1093, 1961
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김성룡,김인선,"로켓엔진 병렬화에 의한 저부가열의 수치적 예측", 한국전산유체공학회지, 제9권 제 3호, 2004.
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김성룡,김인선 "플룸 공기 이원화학종을 이용한 한국형 발사체 클러스터 엔진의 고도별 저부 유동해석", 한국항공우주학회 2010년 추계학술발표회
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http://turbmodels.larc.nasa.go.kr Langley Research Center, Turbulence Modeling Resource
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