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Volumn 1, Issue 2, 1998, Pages 75-88

Numerical investigation of an airfoil with a Gurney flap

Author keywords

[No Author keywords available]

Indexed keywords

ASPECT RATIO; COMPUTER SIMULATION; DRAG; INCOMPRESSIBLE FLOW; LIFT; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; TURBULENT FLOW;

EID: 0032084035     PISSN: 13698869     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1369-8869(98)00010-X     Document Type: Article
Times cited : (102)

References (16)
  • 1
    • 0018017722 scopus 로고
    • Design of subsonic airfoils for high lift
    • Liebeck RH. Design of subsonic airfoils for high lift. Journal of Aircraft 1978;15(9):547-61.
    • (1978) Journal of Aircraft , vol.15 , Issue.9 , pp. 547-561
    • Liebeck, R.H.1
  • 2
    • 0009613215 scopus 로고
    • Inviscid shear flow near the trailing edge of an airfoil
    • Kuchemann D. Inviscid shear flow near the trailing edge of an airfoil. Z. Flugwiss, 1967;15:292-4.
    • (1967) Z. Flugwiss , vol.15 , pp. 292-294
    • Kuchemann, D.1
  • 3
    • 0024621798 scopus 로고
    • Effect of 90 degree flap on the aerodynamics of a two element airfoil
    • Katz J, Largman R. Effect of 90 degree flap on the aerodynamics of a two element airfoil. Journal of Fluids Engineering 1989;111:93-4.
    • (1989) Journal of Fluids Engineering , vol.111 , pp. 93-94
    • Katz, J.1    Largman, R.2
  • 5
    • 0348215377 scopus 로고
    • New designs for improved aerodynamic stability on recent Aerospatiale helicopters
    • Roesch P, Vuillet A. New designs for improved aerodynamic stability on recent Aerospatiale helicopters. Vertica 1982;6:145-64.
    • (1982) Vertica , vol.6 , pp. 145-164
    • Roesch, P.1    Vuillet, A.2
  • 8
    • 0002360198 scopus 로고
    • Innovation with computational aerodynamics: The divergent trailing edge airfoil
    • New York: AIAA
    • Hemme PA. Innovation with computational aerodynamics: the divergent trailing edge airfoil. Applied Computational Aerodynamics. New York: AIAA, 1990, 221-61.
    • (1990) Applied Computational Aerodynamics , pp. 221-261
    • Hemme, P.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.