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Volumn , Issue , 1996, Pages

Evaluation of aft skirt length effects on rocket motor base heat using computational fluid dynamics

Author keywords

[No Author keywords available]

Indexed keywords

FLUID DYNAMICS; HEAT CONVECTION; HEAT TRANSFER; NAVIER STOKES EQUATIONS; PROPULSION; ROCKET ENGINES;

EID: 84961960690     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (10)

References (14)
  • 3
    • 84961915737 scopus 로고
    • Preliminary Assessment of STME Turbulent Exhaust Effect on NLS Base Heating
    • CPIA Publication 595, February
    • Kummerer, K. R. and Eramo, R. S., “Preliminary Assessment of STME Turbulent Exhaust Effect on NLS Base Heating,” 20th JANNAF Exhaust Plume Technology Subcommittee Meeting, CPIA Publication 595, Volume 1, February 1993.
    • (1993) 20Th JANNAF Exhaust Plume Technology Subcommittee Meeting , vol.1
    • Kummerer, K.R.1    Eramo, R.S.2
  • 6
    • 84962898535 scopus 로고
    • Three-Dimensional End-to-End Simulation of Missile Plume/Aerodynamic Flowfields: Part 1 - Methodology & Base Region Studies
    • CPIA Publication 621, October
    • Dash, S. M., Lee, R. A., Sinha, N., and York, B. J., “Three-Dimensional End-to-End Simulation of Missile Plume/Aerodynamic Flowfields: Part 1 - Methodology & Base Region Studies,” 21st JANNAF Exhaust Plume Technology Subcommittee Meeting, CPIA Publication 621, Volume 2, October 1994.
    • (1994) 21St JANNAF Exhaust Plume Technology Subcommittee Meeting , vol.2
    • Dash, S.M.1    Lee, R.A.2    Sinha, N.3    York, B.J.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.