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Volumn 1, Issue , 2004, Pages 133-140

An approach to induced drag reduction and its experimental evaluation

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; BOUNDARY ELEMENT METHOD; COMPUTER SIMULATION; DRAG; FUEL CONSUMPTION; MANEUVERABILITY; OPTIMIZATION; PRESSURE DISTRIBUTION; REYNOLDS NUMBER; TURBULENT FLOW; WIND TUNNELS;

EID: 16244418386     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (8)

References (15)
  • 1
    • 0035472772 scopus 로고    scopus 로고
    • Adaptive wing and flow control technology
    • E. Stanewsky. Adaptive wing and flow control technology. Progress in Aerospace Sciences, 37:583-667, 2001.
    • (2001) Progress in Aerospace Sciences , vol.37 , pp. 583-667
    • Stanewsky, E.1
  • 2
    • 0032669532 scopus 로고    scopus 로고
    • Design concept of a high-altitude longendurance unmanned aerial vehicle
    • Z. Goraj, A. Frydrychiewicz, and J. Winiecki. Design concept of a high-altitude longendurance unmanned aerial vehicle. Aircraft Design, 2:19-44, 1999.
    • (1999) Aircraft Design , vol.2 , pp. 19-44
    • Goraj, Z.1    Frydrychiewicz, A.2    Winiecki, J.3
  • 3
    • 0006340092 scopus 로고
    • Reduction of structural loads using maneuver load control on the advanced fighter technology integration (AFTI) mission adaptive wing
    • NASA
    • S. V. Thornton. Reduction of structural loads using maneuver load control on the advanced fighter technology integration (AFTI) mission adaptive wing. Technical Report TM-4526, NASA, 1993.
    • (1993) Technical Report , vol.TM-4526
    • Thornton, S.V.1
  • 5
    • 16244388043 scopus 로고    scopus 로고
    • Maneuver trim optimization techniques for active aeroelastic wings
    • P. S. Zink, D. N. Mavris, and D. E. Raveh. Maneuver trim optimization techniques for active aeroelastic wings. AIAA paper 2000-1330, 2000.
    • (2000) AIAA Paper 2000-1330 , vol.2000 , Issue.1330
    • Zink, P.S.1    Mavris, D.N.2    Raveh, D.E.3
  • 6
    • 0037529037 scopus 로고    scopus 로고
    • Aeroelastic wing with leading- And trailingedge control surfaces
    • E. H. Dowell, D. B. Bliss, and R. L. Clark. Aeroelastic wing with leading- and trailingedge control surfaces. Journal of Aircraft, 40(3):559-565, 2003.
    • (2003) Journal of Aircraft , vol.40 , Issue.3 , pp. 559-565
    • Dowell, E.H.1    Bliss, D.B.2    Clark, R.L.3
  • 7
    • 0034226416 scopus 로고    scopus 로고
    • The active aeroelastic wing flight research program: Technical program and model analytical development
    • E. Pendleton, D. Bessette, P. Field, G. Miller, and K. Griffin. The active aeroelastic wing flight research program: Technical program and model analytical development. Journal of Aircraft, 37(4):554-561, 2000.
    • (2000) Journal of Aircraft , vol.37 , Issue.4 , pp. 554-561
    • Pendleton, E.1    Bessette, D.2    Field, P.3    Miller, G.4    Griffin, K.5
  • 10
    • 16244416967 scopus 로고    scopus 로고
    • An unsteady aerodynamic boundary element method for applications in aeronautics
    • KTH Aeronautics & Vehicle Engineering
    • D. Eller. An unsteady aerodynamic boundary element method for applications in aeronautics. Technical Report TRITA/AVE 2003:24, KTH Aeronautics & Vehicle Engineering, 2003.
    • (2003) Technical Report TRITA/AVE 2003:24
    • Eller, D.1
  • 15
    • 0024552399 scopus 로고
    • XFOIL: An analysis and design system for low Reynolds number airfoils
    • University of Notre Dame, June
    • M. Drela. XFOIL: An analysis and design system for low Reynolds number airfoils. In Conference on Low Reynolds Number Airfoil Aerodynamics. University of Notre Dame, June 1989.
    • (1989) Conference on Low Reynolds Number Airfoil Aerodynamics
    • Drela, M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.