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Volumn , Issue , 2004, Pages 209-221

Rapid, complete nozzle exhaust gas measurement capability for gas turbine engines

Author keywords

Continuous sweep; Gas turbine engine emissions; Multiple gas analysis system

Indexed keywords

CONTINUOUS SWEEP; GAS TURBINE ENGINE EMISSIONS; MULTIPLE-GAS ANALYSIS SYSTEM; THROTTLE TRANSIENTS;

EID: 23844528851     PISSN: 15588041     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (5)

References (6)
  • 1
    • 0942304033 scopus 로고
    • Procedure for the continuous sampling and measurement of gaseous emissions from aircraft turbine engines
    • Society of Automotive Engineers, Warrendale, PA, August
    • "Procedure for the Continuous Sampling and Measurement of Gaseous Emissions from Aircraft Turbine Engines," Aerospace Recommended Practice ARP1256, Rev. B, Society of Automotive Engineers, Warrendale, PA, August 1990.
    • (1990) Aerospace Recommended Practice ARP1256, Rev. B
  • 4
    • 10644245700 scopus 로고    scopus 로고
    • Procedure for the analysis and evaluation of gaseous emissions from gas turbine engines
    • Society of Automotive Engineers, Warrendale, PA, April
    • "Procedure for the Analysis and Evaluation of Gaseous Emissions from Gas Turbine Engines," Aerospace Recommended Practice ARP1533A, Society of Automotive Engineers, Warrendale, PA, April 2004.
    • (2004) Aerospace Recommended Practice ARP1533A


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.