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Volumn 3, Issue , 2006, Pages 1494-1511

Aerodynamic design studies of conventional & unconventional wings with winglets

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DRAG; OPTIMIZATION; PRESSURE DISTRIBUTION; STRUCTURAL LOADS;

EID: 33845440834     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-3460     Document Type: Conference Paper
Times cited : (16)

References (34)
  • 5
    • 0022026051 scopus 로고
    • Wing design with attainable leading-edge thrust considerations
    • Marc
    • CARLSON, H.W., SHROUT, S.L., & DARDEN, C.M., "Wing Design with Attainable Leading-Edge Thrust Considerations"., AIAA Jo. of Aircraft, Vol.22, No.3, pp 244-8, Marc 1985.
    • (1985) AIAA Jo. of Aircraft , vol.22 , Issue.3 , pp. 244-248
    • Carlson, H.W.1    Shrout, S.L.2    Darden, C.M.3
  • 8
    • 0006141924 scopus 로고
    • A vortex lattice method for the mean camber shapes of trimmed noncoplanar trimmed planforms with minimum vortex drag
    • LAMAR, J.E., "A vortex Lattice Method for the mean Camber shapes of Trimmed Noncoplanar Trimmed Planforms with Minimum Vortex Drag", NASA TN D-8090, 1976.
    • (1976) NASA TN D-8090
    • Lamar, J.E.1
  • 9
    • 33845407434 scopus 로고    scopus 로고
    • The design of manoeuvrable" wings using panel methods, attained thrust & euler codes
    • NANGIA, R.K., "The Design of Manoeuvrable" Wings using Panel Methods, Attained Thrust & Euler Codes", ICAS-92.
    • ICAS-92
    • Nangia, R.K.1
  • 12
    • 33751239834 scopus 로고    scopus 로고
    • Low speed performance optimisation of advanced supersonic civil transport with different le & TE devices
    • Toulouse, France, Oct.94
    • NANGIA, R.K., "Low Speed Performance Optimisation of Advanced Supersonic Civil Transport with Different LE & TE Devices", EAC'94, Toulouse, France, Oct.94.
    • EAC'94
    • Nangia, R.K.1
  • 13
    • 20744445928 scopus 로고    scopus 로고
    • Vortex flow dilemmas & control on wing planforms for high speeds
    • Loen, Norway, May
    • NANGIA, R.K. & MILLER, A.S. "Vortex Flow Dilemmas & Control on Wing Planforms for High Speeds", RTO AVT Symposium, Loen, Norway, May 2001.
    • (2001) RTO AVT Symposium
    • Nangia, R.K.1    Miller, A.S.2
  • 16
    • 20744435749 scopus 로고    scopus 로고
    • Towards design of long-range supersonic military aircraft
    • Providence Rhode Island, USA
    • NANGIA, R.K., PALMER, M.E. & IWANSKI, K.P. (AFRL), "Towards Design of Long-range Supersonic Military Aircraft", AIAA Paper, 2004-5071, Providence Rhode Island, USA, 2004.
    • (2004) AIAA Paper , vol.2004 , Issue.5071
    • Nangia, R.K.1    Palmer, M.E.2    Iwanski, K.P.3
  • 17
    • 20744447188 scopus 로고    scopus 로고
    • Towards design of mach 1.6+ cruise aircraft
    • Providence, RI, USA
    • NANGIA, R.K., PALMER, M.E. & DOE, R.H., "Towards Design of Mach 1.6+ Cruise Aircraft", AIAA Paper, 2004-5070, Providence, RI, USA, 2004
    • (2004) AIAA Paper , vol.2004 , Issue.5070
    • Nangia, R.K.1    Palmer, M.E.2    Doe, R.H.3
  • 19
    • 2942740195 scopus 로고    scopus 로고
    • Design of conventional & unconventional wings for UAV's
    • "UV for Aerial & Naval Military Operations", Ankara, Turkey, Oct.
    • NANGIA, R.K., PALMER, M.E. & GREENWELL. D.I., "Design of Conventional & Unconventional Wings for UAV's", RTO-AVT Symposium, "UV for Aerial & Naval Military Operations", Ankara, Turkey, Oct. 2000.
    • (2000) RTO-AVT Symposium
    • Nangia, R.K.1    Palmer, M.E.2    Greenwell, D.I.3
  • 22
    • 28844454577 scopus 로고    scopus 로고
    • Towards design and optimisation of unconventional high aspect ratio joined-wing type aircraft configurations
    • June Cambridge UK
    • NANGIA, R.K., PALMER, M.E. & TILMANN, C.P., "Towards Design and Optimisation of Unconventional High Aspect Ratio Joined-Wing Type Aircraft Configurations", CEAS Conference, June 2002, Cambridge UK.
    • (2002) CEAS Conference
    • Nangia, R.K.1    Palmer, M.E.2    Tilmann, C.P.3
  • 23
    • 2942750804 scopus 로고    scopus 로고
    • On design of unconventional high aspect ratio joined-wing type aircraft configurations
    • Toronto, Canada
    • NANGIA, R.K., PALMER, M.E. & TILMANN, C.P., "On Design of Unconventional High Aspect Ratio Joined-Wing Type Aircraft Configurations", ICAS 2002-25R2, Toronto, Canada.
    • ICAS 2002-25R2
    • Nangia, R.K.1    Palmer, M.E.2    Tilmann, C.P.3
  • 26
    • 84896375116 scopus 로고    scopus 로고
    • Towards designing novel high-altitude joined-wing sensor-craft (HALE-UAV)
    • AIAA/ICAS Wright Brothers. Centennial, Dayton, OH, USA, July
    • NANGIA, R.K., "Towards Designing Novel High-Altitude Joined-Wing Sensor-Craft (HALE-UAV)", AIAA Paper 2003-2695, AIAA/ICAS Wright Brothers. Centennial, Dayton, OH, USA, July 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.2695
    • Nangia, R.K.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.