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Volumn 1, Issue , 2007, Pages 92-109

Flight testing of Mission Adaptive Compliant Wing

Author keywords

[No Author keywords available]

Indexed keywords

FUEL SAVINGS; TRAILING EDGE FLAPS; WEIGHT SAVINGS;

EID: 34547547871     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (96)

References (8)
  • 3
    • 34547495801 scopus 로고    scopus 로고
    • Reed, S.A., High Altitude Long Endurance Airfoil Performance Validation, WL-TR-96-3091, Flight Dynamics Directorate, Wright Laboratory, Wright-Patterson AFB, OH, January 1996.
    • Reed, S.A., "High Altitude Long Endurance Airfoil Performance Validation", WL-TR-96-3091, Flight Dynamics Directorate, Wright Laboratory, Wright-Patterson AFB, OH, January 1996.
  • 4
    • 0023421355 scopus 로고
    • Two-Dimensional Transonic Aerodynamic Design Method
    • Giles, M. B., and Drela, M., "Two-Dimensional Transonic Aerodynamic Design Method," AIAA Journal, Vol. 25, No. 9, 1987, pp. 1199-1206.
    • (1987) AIAA Journal , vol.25 , Issue.9 , pp. 1199-1206
    • Giles, M.B.1    Drela, M.2
  • 7
    • 0025056224 scopus 로고
    • The Development and Design Integration of a Variable Camber Wing for Long/Medium Range Aircraft
    • November
    • Greff, E., "The Development and Design Integration of a Variable Camber Wing for Long/Medium Range Aircraft", Aeronautical Journal, November 1990.
    • (1990) Aeronautical Journal
    • Greff, E.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.