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Volumn , Issue , 2003, Pages

Development of UAV wings - Subsonic designs

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; COMPUTATIONAL FLUID DYNAMICS; DESIGN; UNMANNED AERIAL VEHICLES (UAV);

EID: 85088757387     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-603     Document Type: Conference Paper
Times cited : (25)

References (19)
  • 1
    • 0001182501 scopus 로고
    • Elements of Airfoil Design Methodology
    • Progress in Astronautics and Aeronautics
    • Drela M., "Elements of Airfoil Design Methodology, " Applied Computational Aerodynamics, Progress in Astronautics and Aeronautics, Vol. 125, 1990.
    • (1990) Applied Computational Aerodynamics , vol.125
    • Drela, M.1
  • 4
    • 0002701463 scopus 로고
    • MIT Computational Aerospace Laboratory, May
    • Drela M., "A User's Guide to MSES V2. 6, " MIT Computational Aerospace Laboratory, May, 1994.
    • (1994) A User's Guide to MSES V2. 6
    • Drela, M.1
  • 12
    • 0024606197 scopus 로고
    • Design and Experimental Results for a High-Altitude, Long-Endurance Airfoil
    • Maughmer, M. D. and Somers, D. M., "Design and Experimental Results for a High-Altitude, Long-Endurance Airfoil, " J. Aircraft, vol. 26, No. 2, 1989.
    • (1989) J. Aircraft , vol.26 , Issue.2
    • Maughmer, M.D.1    Somers, D.M.2
  • 17
    • 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
  • 19
    • 0024056432 scopus 로고
    • Low-Reynolds-Number Airfoil Design for the M.I.T. Daedalus Prototype: A Case Study
    • August
    • M. Drela, "Low-Reynolds-Number Airfoil Design for the M. I. T. Daedalus Prototype: A Case Study, " J. Aircraft, Vol. 25, No. 8, August 1988.
    • (1988) J. Aircraft , vol.25 , Issue.8
    • Drela, M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.