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Volumn 43, Issue 4, 2006, Pages 932-940

Civil-transport wing design concept exploiting new technologies

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MANUFACTURE; COST EFFECTIVENESS; LAMINAR FLOW; STRUCTURAL DESIGN; WINGS;

EID: 33748062996     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.15556     Document Type: Article
Times cited : (23)

References (20)
  • 1
    • 0031145793 scopus 로고    scopus 로고
    • Future large aircraft design - The delta with suction
    • May
    • Denning, R. M., Allen, J. E., and Armstrong, F. W., "Future Large Aircraft Design - the Delta with Suction," The Aeronautical Journal, Vol. 2212, May 1997, pp. 187-198.
    • (1997) The Aeronautical Journal , vol.2212 , pp. 187-198
    • Denning, R.M.1    Allen, J.E.2    Armstrong, F.W.3
  • 4
    • 33748082210 scopus 로고
    • Hybrid laminar flow control study final technical report
    • Oct.
    • Boeing Commercial Airplane Co., "Hybrid Laminar Flow Control Study Final Technical Report," NASA CR 165930, Oct. 1982.
    • (1982) NASA CR 165930
  • 5
    • 84884957076 scopus 로고
    • The correlation between linear stability analysis and cross flow transition near an attachment line
    • Dec.
    • Atkin, C. J., and Poll, D. I. A., "The Correlation Between Linear Stability Analysis and Cross Flow Transition near an Attachment Line," Colloquium on Transitional Boundary Layers in Aeronautics, Dec. 1995.
    • (1995) Colloquium on Transitional Boundary Layers in Aeronautics
    • Atkin, C.J.1    Poll, D.I.A.2
  • 6
    • 33748029045 scopus 로고
    • Ph.D. Dissertation, Dept. of Air Vehicle Design, CoA/Cranfield Univ., Cranfield, England, U.K.
    • Rao, A. J., "Variable Camber Wing for a Transport Aircraft," Ph.D. Dissertation, Dept. of Air Vehicle Design, CoA/Cranfield Univ., Cranfield, England, U.K., 1989.
    • (1989) Variable Camber Wing for a Transport Aircraft
    • Rao, A.J.1
  • 7
    • 0026106482 scopus 로고
    • Forward sweep-a favourable concept for a laminar flow wing
    • Redeker, G., and Wichmann, G., "Forward Sweep-a Favourable Concept for a Laminar Flow Wing," Journal of Aircraft, Vol. 28, No. 2, 1991, pp. 97-102.
    • (1991) Journal of Aircraft , vol.28 , Issue.2 , pp. 97-102
    • Redeker, G.1    Wichmann, G.2
  • 8
    • 85072443692 scopus 로고    scopus 로고
    • Project design studies on aircraft employing natural and assisted laminar flow technologies
    • Wilson, R. A. L., and Jones, R. I., "Project Design Studies on Aircraft Employing Natural and Assisted Laminar Flow Technologies," Society of Automotive Engineers, Paper 952038, 1996.
    • (1996) Society of Automotive Engineers, Paper 952038
    • Wilson, R.A.L.1    Jones, R.I.2
  • 9
    • 33748059448 scopus 로고
    • Study of methods and philosophies for designing laminar flow wings
    • Bedford, England, U.K., Aug.
    • Wong, P. W. C., and Maina, M., "Study of Methods and Philosophies for Designing Laminar Flow Wings," ARA, Contractor Report M275/1, Bedford, England, U.K., Aug. 1995.
    • (1995) ARA, Contractor Report , vol.M275-1
    • Wong, P.W.C.1    Maina, M.2
  • 10
    • 33748071367 scopus 로고
    • Natural laminar flow airfoil analysis and trade studies final report
    • Aug.-June
    • Boeing Commercial Airplane Co., "Natural Laminar Flow Airfoil Analysis and Trade Studies Final Report," NASA CR 159029, Aug. 1977-June 1979.
    • (1977) NASA CR 159029
  • 12
    • 84888840597 scopus 로고
    • High-lift flaps for natural laminar flow airfoils
    • Morgan, H. L., "High-Lift Flaps for Natural Laminar Flow Airfoils," NASA CP-2413, 1985.
    • (1985) NASA CP-2413
    • Morgan, H.L.1
  • 14
    • 0025400180 scopus 로고
    • Laminar flow control leading-edge systems in simulated airline service
    • Wagner, R. D., Maddalon, D. V., and Fisher, D. F., "Laminar Flow Control Leading-Edge Systems in Simulated Airline Service," Journal of Aircraft, Vol. 27, No. 3, 1990.
    • (1990) Journal of Aircraft , vol.27 , Issue.3
    • Wagner, R.D.1    Maddalon, D.V.2    Fisher, D.F.3
  • 15
    • 84888846702 scopus 로고
    • Evaluation of laminar flow control system concepts for subsonic commercial transport aircraft
    • Douglas Aircraft Co. Staff, "Evaluation of Laminar Flow Control System Concepts for Subsonic Commercial Transport Aircraft," NASA CR-159251, 1983.
    • (1983) NASA CR-159251
  • 17
    • 33748071367 scopus 로고
    • Natural laminar flow airfoil analysis and trade studies final report
    • Aug.-June
    • Boeing Commercial Airplane Co., "Natural Laminar Flow Airfoil Analysis and Trade Studies Final Report," NASA CR 159029, Aug. 1977-June 1979.
    • (1977) NASA CR 159029
  • 18
    • 0024096911 scopus 로고
    • A Transonic interactive boundary-layer theory for laminar and turbulent flow over swept wings
    • Woodson, S. H., and DeJarnette, R., "A Transonic Interactive Boundary-Layer Theory for Laminar and Turbulent Flow Over Swept Wings," NASA CR 4185, 1988.
    • (1988) NASA CR 4185
    • Woodson, S.H.1    DeJarnette, R.2
  • 19
    • 33748051932 scopus 로고    scopus 로고
    • Comparative study between inviscid and viscous computations of transonic limit cycle oscillations for a swept-back supercritical airfoil
    • Hussein, A. S., "Comparative Study Between Inviscid and Viscous Computations of Transonic Limit Cycle Oscillations for a Swept-back Supercritical Airfoil," The International Journal of Intelligent Computing and Information Sciences (IJICIS), Vol. 4, No. 1, 2004, pp. 48-66.
    • (2004) The International Journal of Intelligent Computing and Information Sciences (IJICIS) , vol.4 , Issue.1 , pp. 48-66
    • Hussein, A.S.1
  • 20
    • 0036756981 scopus 로고    scopus 로고
    • Numerical investigation of slat and compressibility effects for a high-lift wing
    • Baker, M. D., Mathias, D. L., Roth, K. R., and Cummings, R. M., "Numerical Investigation of Slat and Compressibility Effects for a High-Lift Wing," Journal of Aircraft, Vol. 39, No. 5, 2002, pp. 876-884.
    • (2002) Journal of Aircraft , vol.39 , Issue.5 , pp. 876-884
    • Baker, M.D.1    Mathias, D.L.2    Roth, K.R.3    Cummings, R.M.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.