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Volumn , Issue , 2005, Pages 6993-7004

Development of UAV wings - Transonic designs

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRFOILS; MANEUVERABILITY; SENSITIVITY ANALYSIS; SUBSONIC AERODYNAMICS; WINGS;

EID: 30744439821     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-42     Document Type: Conference Paper
Times cited : (4)

References (18)
  • 3
    • 84888776017 scopus 로고
    • Newton solution of coupled viscous-inviscid multi-element airfoil flow
    • AIAA 90-1470, Seattle, WA, June
    • Drela M., "Newton Solution of Coupled Viscous-Inviscid Multi-Element Airfoil Flow", AIAA 90-1470, AIAA Fluid Dynamics, Plasmodynamics and Laser Conference, Seattle, WA, June 1990.
    • (1990) AIAA Fluid Dynamics, Plasmodynamics and Laser Conference
    • Drela, M.1
  • 4
    • 0002701463 scopus 로고    scopus 로고
    • MIT Computational Aerospace Laboratory, September
    • Drela M., "A User's Guide to MSES 2.95", MIT Computational Aerospace Laboratory, September 1996.
    • (1996) A User's Guide to MSES 2.95
    • Drela, M.1
  • 8
    • 30744453149 scopus 로고
    • September
    • also AIAA Paper 74-1018, September, 1974.
    • (1974) AIAA Paper , vol.74 , Issue.1018
  • 9
    • 0004860511 scopus 로고
    • NASA supercritical airfoils
    • Harris, D.C., "NASA Supercritical Airfoils", NACA Technical Paper 2969, 1990.
    • (1990) NACA Technical Paper , vol.2969
    • Harris, D.C.1
  • 10
    • 30744467063 scopus 로고
    • Low-speed aerodynamic characteristics of a 17-persent-thick medium-speed airfoil designed for general aviation applications
    • McGhee, R.J. and Beasley, W.D.. "Low-Speed Aerodynamic Characteristics of a 17-Persent-Thick Medium-Speed Airfoil Designed for General Aviation Applications", NACA Technical Paper 1786, 1980.
    • (1980) NACA Technical Paper , vol.1786
    • McGhee, R.J.1    Beasley, W.D.2
  • 11
    • 0008564616 scopus 로고
    • Effects of upper surface modification on the aerodynamic characteristics of the NACA 632-215 airfoil section
    • Hicks, R.M. and Schairer, E.T.. "Effects of Upper Surface Modification on the Aerodynamic Characteristics of the NACA 632-215 Airfoil Section", NACA TM78503, 1979.
    • (1979) NACA TM78503
    • Hicks, R.M.1    Schairer, E.T.2
  • 12
    • 85040285086 scopus 로고
    • Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section
    • McGhee, R.J. and Beasley, W.D.. "Wind-Tunnel Results for a Modified 17-Percent-Thick Low-Speed Airfoil Section", NACA Technical Paper 1919, 1981.
    • (1981) NACA Technical Paper , vol.1919
    • McGhee, R.J.1    Beasley, W.D.2
  • 16
    • 0018544669 scopus 로고
    • Transition in the infinite swept attachment line boundary layer
    • Poll, D.I.A.: "Transition in the Infinite Swept Attachment Line Boundary Layer". The Aeronautical Quart., Vol. 30, 1979, pp.607-629.
    • (1979) The Aeronautical Quart. , vol.30 , pp. 607-629
    • Poll, D.I.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.