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Volumn , Issue , 2002, Pages

The effects of swirl injector design on hybrid flame-holding combustion instability

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION CHAMBERS; ENGINES; FUEL INJECTION; NITROGEN OXIDES; PRECOMBUSTION; PROPULSION; RADIAL FLOW; ROCKETS; SUPERSONIC AERODYNAMICS;

EID: 85087601524     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-3578     Document Type: Conference Paper
Times cited : (21)

References (7)
  • 6
    • 84896860427 scopus 로고    scopus 로고
    • The Development of a Hybrid Rocket Engine Test System for Use in Combustion Stability Research
    • April 4-6
    • Pucci, J. M. "The Development of a Hybrid Rocket Engine Test System for Use in Combustion Stability Research. " AIAA Region VI Student Conference, April 4-6, 2002.
    • (2002) AIAA Region VI Student Conference
    • Pucci, J.M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.