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Volumn 5, Issue 7, 2001, Pages 445-455

Realization of an optimized wing camber by using formvariable flap structures

Author keywords

Adaptive wing; Adaptronic; Differential camber variation; Formvariable flap; Multifunctional materials; Smart structures; Variable camber

Indexed keywords


EID: 0035599181     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1270-9638(01)01118-X     Document Type: Article
Times cited : (142)

References (15)
  • 4
    • 0006282154 scopus 로고
    • VDI Verlag, Düsseldorf, ISBN 3-18-400816-9
    • Bölkow L., Ein Jahrhundert Flugzeuge, VDI Verlag, Düsseldorf, 1990, ISBN 3-18-400816-9.
    • (1990) Ein Jahrhundert Flugzeuge
    • Bölkow, L.1
  • 5
    • 0025056224 scopus 로고
    • The development and design integration of a variable camber wing for long/medium range aircraft
    • Greff E., The development and design integration of a variable camber wing for long/medium range aircraft, Aeronaut. J. (1990) 301-310.
    • (1990) Aeronaut. J. , pp. 301-310
    • Greff, E.1
  • 6
    • 0010363256 scopus 로고
    • Variable wing camber control for civil transport aircraft
    • Toulouse
    • Hilbig H., Wagner H., Variable wing camber control for civil transport aircraft, in: ICAS Procedings, ICAS-84-5.2.1, Toulouse, 1984, pp. 107-112.
    • (1984) ICAS Procedings, ICAS-84-5.2.1 , pp. 107-112
    • Hilbig, H.1    Wagner, H.2
  • 13
    • 0026617486 scopus 로고
    • The use of variable camber to reduce drag, weight and costs of transport aircraft
    • Spillman J.J., The use of variable camber to reduce drag, weight and costs of transport aircraft. Aeronaut. J. 96 (951) (1992) 1-9.
    • (1992) Aeronaut. J. , vol.96 , Issue.951 , pp. 1-9
    • Spillman, J.J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.