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Volumn 156, Issue 9, 2009, Pages 1683-1697

Thermoacoustic limit cycles in a premixed laboratory combustor with open and choked exits

Author keywords

Premixed combustion; Thermoacoustic instability

Indexed keywords

ACOUSTIC VELOCITY; ENTROPY FLUCTUATIONS; EQUIVALENCE RATIOS; FLAME DYNAMICS; FLAME HOLDER; FLAME MODELS; FLAMMABILITY LIMITS; HEAT RELEASE FLUCTUATIONS; HIGH-SPEED; INTERACTION INDEX; LIMIT CYCLE; LOW FREQUENCY; OPERATING CONDITION; PREMIXED; PREMIXED COMBUSTION; THEORETICAL INVESTIGATIONS; THERMO-ACOUSTIC MODEL; THERMOACOUSTIC INSTABILITY; THERMOACOUSTICS; TURBULENT PREMIXED FLAME; VELOCITY FLUCTUATIONS;

EID: 68049146033     PISSN: 00102180     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.combustflame.2009.05.011     Document Type: Article
Times cited : (83)

References (68)
  • 1
    • 85002584837 scopus 로고
    • Keller J.J. AIAA J. 33 12 (1995) 2280-2287
    • (1995) AIAA J. , vol.33 , Issue.12 , pp. 2280-2287
    • Keller, J.J.1
  • 17
    • 0003932575 scopus 로고
    • Butterworths Science Publication
    • Crocco L., and Cheng S.L. Theory of Combustion Instability in Liquid Propellant Rocket Motors. AGARDOGRAPH 8 (1956), Butterworths Science Publication
    • (1956) AGARDOGRAPH , vol.8
    • Crocco, L.1    Cheng, S.L.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.