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Volumn , Issue , 1997, Pages

An MDO investigation of the impact of practical constraints on an HSCT configuration

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; PLANFORMS;

EID: 84983146275     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (4)

References (49)
  • 1
  • 5
    • 0028257638 scopus 로고
    • Variable-Complexity Aerodynamic Optimization of a High Speed Civil Transport Wing
    • January-Febuary
    • Hutchison, M. G., Unger, E., Mason, W. H., Grossman, B., and Haftka, R. T., "Variable-Complexity Aerodynamic Optimization of a High Speed Civil Transport Wing," Journal of Aircraft, vol. 31, pp. 110-116, January-Febuary 1994.
    • (1994) Journal of Aircraft , vol.31 , pp. 110-116
    • Hutchison, M.G.1    Unger, E.2    Mason, W.H.3    Grossman, B.4    Haftka, R.T.5
  • 10
    • 0029341258 scopus 로고
    • Subsonic Wing Planform Design Using Multidisciplinary Optimization
    • July-August
    • Wakayama, S. and Kroo, L, "Subsonic Wing Planform Design Using Multidisciplinary Optimization," Journal of Aircraft, vol. 32, pp. 746-753, July-August 1990.
    • (1990) Journal of Aircraft , vol.32 , pp. 746-753
    • Wakayama, S.1    Kroo, L.2
  • 11
    • 0027697631 scopus 로고
    • Optimization of Joined-Wing Aircraft
    • November-Decernber
    • Gallman, J. W., Smith, S. C., and Kroo, I. M., "Optimization of Joined-Wing Aircraft," Journal of Aircraft, vol. 30, pp. 897-905, November-Decernber 1993.
    • (1993) Journal of Aircraft , vol.30 , pp. 897-905
    • Gallman, J.W.1    Smith, S.C.2    Kroo, I.M.3
  • 29
    • 84983126630 scopus 로고    scopus 로고
    • AIAA Paper 96-4058, Proceedings of the 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Bellevue, WA, Sept
    • Anderson, M. A. and Mason, W., "An MDO Approach to Control-Configured-Vehicle Design," AIAA Paper 96-4058, Proceedings of the 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Bellevue, WA, pp. 734-743, Sept. 1996. http://www.aoe.vt.edu/aoe/faculty/ Mason_f/MRRpubs96. html.
    • (1996) An MDO Approach to Control-Configured-Vehicle Design , pp. 734-743
    • Anderson, M.A.1    Mason, W.2
  • 33
    • 84983136277 scopus 로고    scopus 로고
    • Washington, DC
    • FAA, Washington, DC, FAR Part 25.
    • FAR Part 25
  • 46
    • 0003963588 scopus 로고
    • Flight Control Division, Air Force Flight Dynamics Laboratory, WPAFB, Ohio, 45433-0000, Revised
    • Hoak, D. E. et al, USAF Stability and Control DATCOM. Flight Control Division, Air Force Flight Dynamics Laboratory, WPAFB, Ohio, 45433-0000, 1978. Revised.
    • (1978) USAF Stability and Control DATCOM
    • Hoak, D.E.1
  • 48
    • 1942498252 scopus 로고
    • NASA Contractor Report 4235
    • Douglas Aircraft Company, "Study of High-Speed Civil Transports," NASA Contractor Report 4235, p. 105, 1989.
    • (1989) Study of High-Speed Civil Transports , pp. 105
  • 49
    • 84983186835 scopus 로고
    • The Influence of Subsonic Mission Segments on the Use of Variable-Sweep Wings for High Speed Civil Transport Configurations
    • Martin, G. L., Beissner Jr., F. L., Domack, C. S., and Shields, E. W., "The Influence of Subsonic Mission Segments on the Use of Variable-Sweep Wings for High Speed Civil Transport Configurations," AIAA Paper 88-4470, Sept. 1988.
    • (1989) AIAA Paper
    • Martin, G.L.1    Beissner Jr, F.L.2    Domack, C.S.3    Shields, E.W.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.