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Volumn , Issue , 1997, Pages

Development of CFD model for simulating gas/liquid injectors in rocket engine design

Author keywords

[No Author keywords available]

Indexed keywords

BOOSTERS (ROCKET); COMPUTATIONAL FLUID DYNAMICS; ENGINES; FLOW OF FLUIDS; MACHINE DESIGN; PROPULSION; ROCKET ENGINES; ROCKETS;

EID: 84962868585     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (6)

References (18)
  • 9
    • 0021445528 scopus 로고
    • Explicit Representations of the Complete Velocity Profile in a Turbulent Boundary Layer
    • June
    • Liakopoulos, A., “Explicit Representations of the Complete Velocity Profile in a Turbulent Boundary Layer,” AIAA Journal, Vol. 22, No. 6, June 1984, pp. 844-846.
    • (1984) AIAA Journal , vol.22 , Issue.6 , pp. 844-846
    • Liakopoulos, A.1
  • 10
    • 0021820459 scopus 로고
    • On the use of Wall Functions as Boundary Conditions for Two-Dimensional Separated Compressible Flows
    • AIAA Paper 85-0180, Jan
    • Viegas, J. R., Rubesin, M. W., and Horstman, C. C., “On the use of Wall Functions as Boundary Conditions for Two-Dimensional Separated Compressible Flows,” AIAA Paper 85-0180, AIAA 23rd Aerospace Sciences Meeting, Jan. 14-17,1985.
    • (1985) AIAA 23Rd Aerospace Sciences Meeting , pp. 14-17
    • Viegas, J.R.1    Rubesin, M.W.2    Horstman, C.C.3
  • 14
    • 84962864171 scopus 로고    scopus 로고
    • Tripropellant Rocket Combustion Using A Mixed RP-1/GH2 Injector
    • Penn State University, Oct. 30-31
    • Mouis A.G.F., Pal, S., and Santoro, R.J., “Tripropellant Rocket Combustion Using A Mixed RP-1/GH2 Injector,” 8th Annual Symposium on Space Propulsion, Penn State University, pp. 55-58, Oct. 30-31, 1996.
    • (1996) 8Th Annual Symposium on Space Propulsion , pp. 55-58
    • Mouis, A.G.F.1    Pal, S.2    Santoro, R.J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.