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Volumn 39, Issue 4, 2002, Pages 654-661

Design and testing of a winglet airfoil for low-speed aircraft

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; CODES (SYMBOLS); DRAG; REYNOLDS NUMBER; WIND TUNNELS;

EID: 0036650998     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2978     Document Type: Article
Times cited : (38)

References (21)
  • 2
    • 85067320097 scopus 로고    scopus 로고
    • The design of winglets for high-performance sailplanes
    • June
    • (2001) AIAA Paper , vol.2001 , Issue.2406
    • Maughmer, M.D.1
  • 18
    • 0003209770 scopus 로고
    • Simplified method for determination of critical height of distributed roughness particles for boundary-layer transition at Mach numbers from 0 to 5
    • Sept.
    • (1958) NACA TN , vol.4363
    • Braslow, A.L.1    Knox, E.C.2
  • 21
    • 0041890817 scopus 로고    scopus 로고
    • An empirical criterion for laminar-to-turbulent boundary-layer transition
    • April
    • (1999) Technical Soaring , vol.23 , Issue.2
    • Eppler, R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.