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Volumn , Issue , 2005, Pages

Benchmark wall heat flux data for a go2/gh2 single element combustor

Author keywords

[No Author keywords available]

Indexed keywords

AMBIENT TEMPERATURES; AXIAL LOCATIONS; CHAMBER PRESSURE; CIRCULAR CROSS-SECTIONS; CO-AXIAL INJECTORS; FLOWRATES; GASEOUS HYDROGEN; GASEOUS OXYGEN; HEAT FLUX GAUGES; HYDROGEN PROPELLANT; INJECTION VELOCITY; MAXIMUM HEAT FLUX; MIXTURE RATIO; MOMENTUM FLUX; PROPELLANT FLOW; REACTION ZONES; SINGLE ELEMENT; WALL HEAT FLUX;

EID: 77957845778     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (65)

References (9)
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    • McBride, B.J.1    Gordon, S.2
  • 4
    • 69249085160 scopus 로고    scopus 로고
    • Omega Engineering, Inc., Temperature Handbook. MM. Revised Thermocouple Reference Tables, Type T Reference Tables N.I.S.T. Monograph 175 Revised to 1TS-90, p. Z-223, 1999.
    • Omega Engineering, Inc., Temperature Handbook. Vol. MM. "Revised Thermocouple Reference Tables, Type T Reference Tables N.I.S.T. Monograph 175 Revised to 1TS-90," p. Z-223, 1999.
  • 5
    • 69249104026 scopus 로고    scopus 로고
    • Omega Engineering. Inc., Temperature Handbook. MM, 1TS-90 Thermocouple Direct and Inverse Polynomials. p. Z-199, 1999.
    • Omega Engineering. Inc., Temperature Handbook. Vol. MM, "1TS-90 Thermocouple Direct and Inverse Polynomials." p. Z-199, 1999.
  • 6
    • 0001798547 scopus 로고
    • Thermocouple Materials
    • March
    • Caldwell, F. R., "Thermocouple Materials," NBS Monograph 40, March 1962.
    • (1962) NBS Monograph , vol.40
    • Caldwell, F.R.1
  • 7
    • 0003961002 scopus 로고    scopus 로고
    • Experimentation and Uncertainty Analysis for Engineers
    • 2nd edition, New York
    • Coleman H. W. and Steele, W. G., Experimentation and Uncertainty Analysis for Engineers, 2nd edition John Wiley and Sons, New York, 1999.
    • (1999) John Wiley and Sons
    • Coleman, H.W.1    Steele, W.G.2
  • 8
    • 77957068260 scopus 로고
    • Turbulent Boundary-Layer Heat Transfer from Rapidly Accelerating Flow of Rocket Combustion Gases and of Hot Air
    • Bartz, D. R., "Turbulent Boundary-Layer Heat Transfer from Rapidly Accelerating Flow of Rocket Combustion Gases and of Hot Air," Advances in Heat Transfer, Vol. 2, 1965.
    • (1965) Advances in Heat Transfer , vol.2
    • Bartz, D.R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.