메뉴 건너뛰기




Volumn 24, Issue 5, 2008, Pages 700-719

Self-sustained aeroelastic oscillations of a NACA0012 airfoil at low-to-moderate Reynolds numbers

Author keywords

Aeroelasticity; LCO; Low Re aerodynamics; NACA0012; Self sustained oscillations

Indexed keywords

AIRFOILS; MIXED CONVECTION; MOTION ESTIMATION; REYNOLDS NUMBER; RHENIUM; SURFACE ROUGHNESS;

EID: 46749089021     PISSN: 08899746     EISSN: 10958622     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2007.11.005     Document Type: Article
Times cited : (158)

References (35)
  • 2
    • 0027626092 scopus 로고
    • Low-frequency flow oscillation over airfoils near stall
    • Bragg M.B., Heinrich D.C., and Khodadoust A. Low-frequency flow oscillation over airfoils near stall. AIAA Journal 31 7 (1993) 1341-1343
    • (1993) AIAA Journal , vol.31 , Issue.7 , pp. 1341-1343
    • Bragg, M.B.1    Heinrich, D.C.2    Khodadoust, A.3
  • 4
    • 0032737997 scopus 로고    scopus 로고
    • Flowfield measurements over an airfoil during natural low-frequency oscillations near stall
    • Broeren A.P., and Bragg M.B. Flowfield measurements over an airfoil during natural low-frequency oscillations near stall. AIAA Journal 37 1 (1998) 130-132
    • (1998) AIAA Journal , vol.37 , Issue.1 , pp. 130-132
    • Broeren, A.P.1    Bragg, M.B.2
  • 8
    • 85002855514 scopus 로고
    • Comment on aeroelastic oscillations caused by transitional boundary layers and their attenuation
    • Ericsson L.E. Comment on aeroelastic oscillations caused by transitional boundary layers and their attenuation. Journal of Aircraft 25 10 (1988) 975-976
    • (1988) Journal of Aircraft , vol.25 , Issue.10 , pp. 975-976
    • Ericsson, L.E.1
  • 9
    • 0025682191 scopus 로고
    • Effects of transition on wind tunnel simulation of vehicle dynamics
    • Ericsson L.E. Effects of transition on wind tunnel simulation of vehicle dynamics. Progress in Aerospace Sciences 27 (1990) 121-144
    • (1990) Progress in Aerospace Sciences , vol.27 , pp. 121-144
    • Ericsson, L.E.1
  • 11
    • 0025486756 scopus 로고
    • Control of low-speed airfoil aerodynamics
    • Gad-el-Hak M. Control of low-speed airfoil aerodynamics. AIAA Journal 28 9 (1990) 1537-1552
    • (1990) AIAA Journal , vol.28 , Issue.9 , pp. 1537-1552
    • Gad-el-Hak, M.1
  • 12
    • 0033314479 scopus 로고    scopus 로고
    • Effects of freestream turbulence on wing-surface flow and aerodynamic performance
    • Huang R.-F., and Lee H.-W. Effects of freestream turbulence on wing-surface flow and aerodynamic performance. Journal of Aircraft 36 6 (1999) 965-972
    • (1999) Journal of Aircraft , vol.36 , Issue.6 , pp. 965-972
    • Huang, R.-F.1    Lee, H.-W.2
  • 13
    • 0033640251 scopus 로고    scopus 로고
    • Turbulence effect on frequency characteristics of unsteady motions in wake of wing
    • Huang R.-F., and Lee H.-W. Turbulence effect on frequency characteristics of unsteady motions in wake of wing. AIAA Journal 38 1 (2000) 85-93
    • (2000) AIAA Journal , vol.38 , Issue.1 , pp. 85-93
    • Huang, R.-F.1    Lee, H.-W.2
  • 14
    • 0029110424 scopus 로고
    • Vortex shedding and shear-layer instability of wing at low-Reynolds numbers
    • Huang R.-F., and Lin C. Vortex shedding and shear-layer instability of wing at low-Reynolds numbers. AIAA Journal 33 8 (1995) 1398-1403
    • (1995) AIAA Journal , vol.33 , Issue.8 , pp. 1398-1403
    • Huang, R.-F.1    Lin, C.2
  • 15
    • 0029656580 scopus 로고    scopus 로고
    • Influence of surface flow on aerodynamic loads of a cantilever wing
    • Huang R.-F., Shy W.W., Lin S.W., and Hsiao F.-B. Influence of surface flow on aerodynamic loads of a cantilever wing. AIAA Journal 34 3 (1996) 527-532
    • (1996) AIAA Journal , vol.34 , Issue.3 , pp. 527-532
    • Huang, R.-F.1    Shy, W.W.2    Lin, S.W.3    Hsiao, F.-B.4
  • 16
    • 46749101580 scopus 로고    scopus 로고
    • Jacobs, E.N., Sherman, A., 1937. Airfoil section characteristics as affected by variations of the Reynolds number. NACA Report 586.
    • Jacobs, E.N., Sherman, A., 1937. Airfoil section characteristics as affected by variations of the Reynolds number. NACA Report 586.
  • 17
    • 46749135903 scopus 로고    scopus 로고
    • Jones, B.M., 1933. An experimental study of the stalling of wings. Aeronautical Research Committee Reports and Memoranda 1588, His Majesty's Stationery Office, London.
    • Jones, B.M., 1933. An experimental study of the stalling of wings. Aeronautical Research Committee Reports and Memoranda 1588, His Majesty's Stationery Office, London.
  • 18
    • 16844387528 scopus 로고    scopus 로고
    • Vortex-shedding characteristics in the wake of an oscillating airfoil at low Reynolds number
    • Jung Y.W., and Park S.O. Vortex-shedding characteristics in the wake of an oscillating airfoil at low Reynolds number. Journal of Fluids and Structures 20 (2005) 451-464
    • (2005) Journal of Fluids and Structures , vol.20 , pp. 451-464
    • Jung, Y.W.1    Park, S.O.2
  • 19
    • 46749109879 scopus 로고    scopus 로고
    • Lambourne, N.C., 1947. An experimental investigation on the flutter characteristics of a model flying wing. British Aeronautical Research Council, Reports and Memoranda 2626.
    • Lambourne, N.C., 1947. An experimental investigation on the flutter characteristics of a model flying wing. British Aeronautical Research Council, Reports and Memoranda 2626.
  • 20
  • 22
    • 0023383703 scopus 로고
    • Aeroelastic oscillations caused by transitional boundary layers and their attenuation
    • Mabey D.G., Ashill P.R., and Welsh B.L. Aeroelastic oscillations caused by transitional boundary layers and their attenuation. Journal of Aircraft 24 7 (1987) 463-469
    • (1987) Journal of Aircraft , vol.24 , Issue.7 , pp. 463-469
    • Mabey, D.G.1    Ashill, P.R.2    Welsh, B.L.3
  • 23
    • 27744568210 scopus 로고    scopus 로고
    • The aeroelastic response of a wing section with a structural freeplay nonlinearity: an experimental investigation
    • Marsden C.C., and Price S.J. The aeroelastic response of a wing section with a structural freeplay nonlinearity: an experimental investigation. Journal of Fluids and Structures 21 (2005) 257-276
    • (2005) Journal of Fluids and Structures , vol.21 , pp. 257-276
    • Marsden, C.C.1    Price, S.J.2
  • 24
    • 46749102391 scopus 로고    scopus 로고
    • McCullough, G.B., Gault, D.E., 1951. Examples of three representative types of airfoil-section stall at low speed. NACA-TN-2502.
    • McCullough, G.B., Gault, D.E., 1951. Examples of three representative types of airfoil-section stall at low speed. NACA-TN-2502.
  • 25
    • 46749115025 scopus 로고    scopus 로고
    • Mueller, T.J., 1985. Low Reynolds number vehicles. AGARD-AG-288.
    • Mueller, T.J., 1985. Low Reynolds number vehicles. AGARD-AG-288.
  • 26
    • 84977108790 scopus 로고    scopus 로고
    • O'Neil, T., Gilliatt, H., Strganac, T., 1996. Investigations of aeroelastic response for a system with continuous structural nonlinearities. In: Proceedings of the 37th AIAA SDM Conference, AIAA Paper 96-1390, Salt Lake City, USA.
    • O'Neil, T., Gilliatt, H., Strganac, T., 1996. Investigations of aeroelastic response for a system with continuous structural nonlinearities. In: Proceedings of the 37th AIAA SDM Conference, AIAA Paper 96-1390, Salt Lake City, USA.
  • 27
    • 0142088881 scopus 로고    scopus 로고
    • Random binary (coalescence) flutter of a two-dimensional linear airfoil
    • Poirel D., and Price S.J. Random binary (coalescence) flutter of a two-dimensional linear airfoil. Journal of Fluids and Structures 18 1 (2003) 23-42
    • (2003) Journal of Fluids and Structures , vol.18 , Issue.1 , pp. 23-42
    • Poirel, D.1    Price, S.J.2
  • 28
    • 46749086498 scopus 로고    scopus 로고
    • Poirel, D., Clément, M., Bouchard, H., Vaivads, R., 2003. Qualification of an experimental aeroelastic apparatus at RMC. In: Proceedings of the CASI Ninth Aerodynamics Symposium, Montréal, Canada.
    • Poirel, D., Clément, M., Bouchard, H., Vaivads, R., 2003. Qualification of an experimental aeroelastic apparatus at RMC. In: Proceedings of the CASI Ninth Aerodynamics Symposium, Montréal, Canada.
  • 29
    • 27144436836 scopus 로고    scopus 로고
    • Flutter-margin method accounting for modal parameter uncertainties
    • Poirel D., Dunn S., and Porter J. Flutter-margin method accounting for modal parameter uncertainties. Journal of Aircraft 42 5 (2005) 1236-1243
    • (2005) Journal of Aircraft , vol.42 , Issue.5 , pp. 1236-1243
    • Poirel, D.1    Dunn, S.2    Porter, J.3
  • 30
    • 0026925165 scopus 로고
    • Flutter and stall response of a helicopter blade with structural nonlinearity
    • Tang D.M., and Dowell E.H. Flutter and stall response of a helicopter blade with structural nonlinearity. Journal of Aircraft 29 5 (1992) 953-960
    • (1992) Journal of Aircraft , vol.29 , Issue.5 , pp. 953-960
    • Tang, D.M.1    Dowell, E.H.2
  • 31
    • 50549221129 scopus 로고
    • Low-speed flows involving bubble separation
    • Tani I. Low-speed flows involving bubble separation. Progress in Aeronautical Sciences 5 (1964) 70-103
    • (1964) Progress in Aeronautical Sciences , vol.5 , pp. 70-103
    • Tani, I.1
  • 32
  • 34
    • 0025414615 scopus 로고
    • Transition from order to chaos in the wake of an airfoil
    • William-Stuber K., and Gharib M. Transition from order to chaos in the wake of an airfoil. Journal of Fluid Mechanics 213 (1990) 29-57
    • (1990) Journal of Fluid Mechanics , vol.213 , pp. 29-57
    • William-Stuber, K.1    Gharib, M.2
  • 35
    • 0024665935 scopus 로고
    • A natural low-frequency oscillation of the flow over an airfoil near stalling conditions
    • Zaman K.B.M.Q., McKinzie D., and Rumsey C. A natural low-frequency oscillation of the flow over an airfoil near stalling conditions. Journal of Fluid Mechanics 202 (1989) 403-442
    • (1989) Journal of Fluid Mechanics , vol.202 , pp. 403-442
    • Zaman, K.B.M.Q.1    McKinzie, D.2    Rumsey, C.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.