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Volumn 192, Issue 1, 2003, Pages 325-354

A multidomain spectral method for supersonic reactive flows

Author keywords

Compressible Navier Stokes equations; Multidomain spectral method; Penalty interface conditions; Recessed cavity flame holder; Supersonic combustor

Indexed keywords

ADAPTIVE FILTERS; MACH NUMBER; NAVIER STOKES EQUATIONS; NUMERICAL METHODS; VISCOUS FLOW;

EID: 0242511111     PISSN: 00219991     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jcp.2003.07.022     Document Type: Article
Times cited : (23)

References (30)
  • 16
    • 85007189112 scopus 로고    scopus 로고
    • Ph.D Thesis, Brown University
    • J.H. Jung, Ph.D. Thesis, Brown University, 2002.
    • (2002)
    • Jung, J.H.1
  • 23
  • 25
    • 85007181309 scopus 로고
    • NASA Technical Memorandum 4436
    • M.B. Tracy, E.B. Plentovish, NASA Technical Memorandum 4436, 1993.
    • (1993)
    • Tracy, M.B.1    Plentovish, E.B.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.