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Volumn 5, Issue , 2004, Pages 3979-3988

A design and analysis of a morphing Hyper-Elliptic Cambered Span (HECS) wing

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC EFFECTS; BENDING STRESSES; CRITICAL FORCE; HYPER-ELLIPTIC CAMBERED SPAN (HECS) WING;

EID: 16244382816     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (36)

References (23)
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  • 4
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    • Oct.
    • Monner, H.P., "Realization of an Optimized Wing Camber by Using Formvariable Flap Structures," Aerospace Science and Technology, Vol. 5, Oct. 2001, pp. 445-455.
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    • Monner, H.P.1
  • 5
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    • Master's Thesis, Virginia Polytechnic Institute & State University, November
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    • (2002) Kinematic Analysis of Tensegrity Structures
    • Whittier, W.B.1
  • 6
    • 84896893614 scopus 로고    scopus 로고
    • Flight dynamic simulation assessment of a morphable hyper-elliptic cambered span winged configuration
    • AIAA Paper 2003-5301, Austin, Texas, August 11-14
    • Davidson, J.B., Chwalowski, P., Lazos, B.S., "Flight Dynamic Simulation Assessment of a Morphable Hyper-Elliptic Cambered Span Winged Configuration," AIAA Paper 2003-5301, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Austin, Texas, August 11-14, 2003.
    • (2003) AIAA Atmospheric Flight Mechanics Conference and Exhibit
    • Davidson, J.B.1    Chwalowski, P.2    Lazos, B.S.3
  • 7
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    • Borst, H.V.1
  • 8
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    • Staufenbiel, R.W.1    Schlichting, U.J.2
  • 11
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    • Computation of in duced drag for elliptical and crescent-shaped wings
    • Smith, S. C., Kroo, I. M., "Computation of In duced Drag for Elliptical and Crescent-Shaped Wings," Journal of Aircraft, Vol. 30, 1993, pp. 446-452.
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    • Smith, S.C.1    Kroo, I.M.2
  • 14
    • 0025464859 scopus 로고
    • Minimum induced drag for wings with spanwise camber
    • July
    • Lowson, M. V., "Minimum Induced Drag for Wings with Spanwise Camber," Journal of Air craft, Vol. 27, July, 1990, pp. 627-631.
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    • Lowson, M.V.1
  • 16
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  • 17
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    • Reduction in induced drag by the use of aft swept wing tips
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    • Burkett, C.W.1
  • 18
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.