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Volumn , Issue , 1998, Pages

Internal flow analysis of a technology demonstrator rocket motor with new CFD code

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINA; ALUMINUM OXIDE; CHEMICAL REACTIONS; CODES (SYMBOLS); COMPUTATIONAL FLUID DYNAMICS; CURVE FITTING; EXPLOSIVES; NUMERICAL METHODS; PROPULSION; ROCKET ENGINES; SOLID PROPELLANTS; TURBULENCE MODELS;

EID: 85085848738     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-3967     Document Type: Conference Paper
Times cited : (3)

References (9)
  • 3
    • 85007694431 scopus 로고
    • Drag Coefficient of Particles in a Rocket Nozzle
    • Crowe, C. T., “Drag Coefficient of Particles in a Rocket Nozzle”, AIAA Journal, 5, 1021-1022, 1967.
    • (1967) AIAA Journal , vol.5 , pp. 1021-1022
    • Crowe, C.T.1
  • 6
    • 0017969563 scopus 로고
    • Reaction Rate Coefficients for Flame Calculations
    • Jensen, D.E., and Jones, G.A., “Reaction Rate Coefficients for Flame Calculations”, Combustion and Flame, 32, 1978.
    • (1978) Combustion and Flame , pp. 32
    • Jensen, D.E.1    Jones, G.A.2
  • 8
    • 77958196941 scopus 로고    scopus 로고
    • Dr. ing.-thesis, Dept. of Applied Mechanics, Thermo-and Fluid Dynamics, The Norwegian Institute of Technology, Trondheim
    • I. J. Øye, “On the Aerothermodynamic Effects on Space Vehicles,” Dr. ing.-thesis, Dept. of Applied Mechanics, Thermo-and Fluid Dynamics, The Norwegian Institute of Technology, Trondheim, 1996”
    • (1996) On the Aerothermodynamic Effects on Space Vehicles
    • Øye, I.J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.