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Volumn 8, Issue , 2006, Pages 5439-5450

Design, manufacturing and preliminary test results of an adaptive wing camber model

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT DYNAMICS; MATHEMATICAL MODELS; NUMERICAL METHODS; OPTIMIZATION; RELIABILITY;

EID: 34147121171     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-2043     Document Type: Conference Paper
Times cited : (25)

References (16)
  • 1
    • 16244418386 scopus 로고    scopus 로고
    • D. Eller, S. H., An Approach to Induced Drag Reduction and its Experimental Evaluation, 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials, Palm Springs, California, AIAA, Wahington, DC, 19-22 April 2004, pp. 184-196.
    • D. Eller, S. H., "An Approach to Induced Drag Reduction and its Experimental Evaluation," 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials, Palm Springs, California, AIAA, Wahington, DC, 19-22 April 2004, pp. 184-196.
  • 2
    • 0035472772 scopus 로고    scopus 로고
    • Adaptive wing and flow control technology
    • edited by H. F. Nelson, AIAA, New York
    • Stanewsky, E., "Adaptive wing and flow control technology," Progress in Aerospace Sciences, edited by H. F. Nelson, Vol. 37, AIAA, New York, 2001, pp. 583-667.
    • (2001) Progress in Aerospace Sciences , vol.37 , pp. 583-667
    • Stanewsky, E.1
  • 3
    • 0006340092 scopus 로고
    • Reduction of structural loads using maneuver load control on the advanced fighter technology integration (AFTI) mission adaptive wing
    • Thornton, S. V., "Reduction of structural loads using maneuver load control on the advanced fighter technology integration (AFTI) mission adaptive wing," Nasa tm-4526, 1993.
    • (1993) Nasa tm-4526
    • Thornton, S.V.1
  • 5
    • 0026617486 scopus 로고
    • The use of variable camber to reduce drag, weight and costs of transport aircraft
    • January
    • Spillman, J. J., "The use of variable camber to reduce drag, weight and costs of transport aircraft," Aeronautical Journal, January 1982, pp. 1-9.
    • (1982) Aeronautical Journal , pp. 1-9
    • Spillman, J.J.1
  • 6
    • 0004825913 scopus 로고
    • The minimum Induced Drag of Airfoils
    • Tech. rep, NASA-TR-121
    • Munk, M. M., "The minimum Induced Drag of Airfoils," Tech. rep., NASA-TR-121, 1921.
    • (1921)
    • Munk, M.M.1
  • 8
    • 0035516874 scopus 로고    scopus 로고
    • Maneuver trim optimization techniques for active aeroelastic wings
    • Nov.-Dec
    • Zink, P. S., Mavris, D. N., and Raveh, D. E., "Maneuver trim optimization techniques for active aeroelastic wings," Journal of Aircraft, Vol. 38, No. 6, Nov.-Dec. 2001, pp. 1139-1146.
    • (2001) Journal of Aircraft , vol.38 , Issue.6 , pp. 1139-1146
    • Zink, P.S.1    Mavris, D.N.2    Raveh, D.E.3
  • 10
    • 0019584841 scopus 로고
    • Mission Adaptive Wing for Tactical Aircraft
    • Gilbert, W. W., "Mission Adaptive Wing for Tactical Aircraft," Journal of Aircraft, Vol. 18, No. 7, 1981, pp. 597-602.
    • (1981) Journal of Aircraft , vol.18 , Issue.7 , pp. 597-602
    • Gilbert, W.W.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.