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Volumn , Issue , 2004, Pages

Applications of flow control to sections designed with upper surface trailing edge separation

Author keywords

[No Author keywords available]

Indexed keywords

ADVERSE PRESSURE GRADIENT; AERO-DYNAMIC PERFORMANCE; AERODYNAMIC RESEARCH; CONVENTIONAL DESIGN; EXPERIMENTAL EVIDENCE; LOW SPEED PERFORMANCE; NATURAL LAMINAR FLOWS; POTENTIAL BENEFITS;

EID: 84897753111     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (1)

References (11)
  • 5
    • 0000250414 scopus 로고
    • Shock-induced separation and its prevention by design and boundary layer control
    • Ed G V Lachmann, Pergamon Press
    • H H Pearcey, "Shock-induced separation and its prevention by design and boundary layer control", in "Boundary layer and flow control", Vol. 2, Ed G V Lachmann, Pergamon Press, 1961, pp 1170-1344.
    • (1961) Boundary Layer and Flow Control , vol.2 , pp. 1170-1344
    • Pearcey, H.H.1
  • 6
    • 84897788591 scopus 로고
    • Vortex generators for control of shock-induced separation
    • ESDU Technical data memorandum 93024
    • "Vortex generators for control of shock-induced separation", "Part1: Introduction and aerodynamics", ESDU Technical data memorandum 93024, 1993.
    • (1993) Part1: Introduction and Aerodynamics


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.