메뉴 건너뛰기




Volumn 25, Issue 4, 2009, Pages 433-450

Analysis of non-symmetrical flapping airfoils

Author keywords

Airfoil; Design of experiments; Flapping; Non symmetrical; Ornithopter

Indexed keywords

FLAPPING; FLAPPING AIRFOILS; IN-BETWEEN; LIFT COEFFICIENT; LIFT FORCE; NON-SYMMETRICAL; ORNITHOPTER; PHASE ANGLES; PROPULSIVE EFFICIENCIES; REDUCED FREQUENCY; RESPONSE SURFACE METHODOLOGY; THRUST COEFFICIENTS;

EID: 67651230672     PISSN: 05677718     EISSN: None     Source Type: Journal    
DOI: 10.1007/s10409-009-0259-1     Document Type: Article
Times cited : (15)

References (26)
  • 1
    • 47749092028 scopus 로고    scopus 로고
    • Computational aerodynamics of low Reynolds number plunging, pitching and flexible wings for MAV applications
    • 10.1007/s10409-008-0164-z
    • W. Shyy Y. Lian J. Tang H. Liu P. Trizila B. Stanford L. Bernal C. Cesnik P. Friedmann P. Ifju 2008 Computational aerodynamics of low Reynolds number plunging, pitching and flexible wings for MAV applications. Acta Mech. Sinica 24 351-373 10.1007/s10409-008-0164-z.
    • (2008) Acta Mech. Sinica , vol.24 , pp. 351-373
    • Shyy, W.1    Lian, Y.2    Tang, J.3    Liu, H.4    Trizila, P.5    Stanford, B.6    Bernal, L.7    Cesnik, C.8    Friedmann, P.9    Ifju, P.10
  • 2
    • 0024732317 scopus 로고
    • Vortical patterns in the wake of an oscillating airfoil
    • M.M. Koochesfahani 1989 Vortical patterns in the wake of an oscillating airfoil. AIAA J. 27 1200-1205.
    • (1989) AIAA J. , vol.27 , pp. 1200-1205
    • Koochesfahani, M.M.1
  • 3
    • 44949266298 scopus 로고
    • Optimal thrust development in oscillating foils with application to fish propulsion
    • G.S. Triantafyllou M.S. Triantafyllou M.A. Grosenbaugh 1993 Optimal thrust development in oscillating foils with application to fish propulsion J. Fluids Struct. 7 205-224.
    • (1993) J. Fluids Struct. , vol.7 , pp. 205-224
    • Triantafyllou, G.S.1    Triantafyllou, M.S.2    Grosenbaugh, M.A.3
  • 4
    • 0142153256 scopus 로고    scopus 로고
    • Flying and swimming animals cruise at a Strouhal number tuned for high power efficiency
    • 10.1038/nature02000
    • G.K. Taylor R.L. Nudds A.L.R. Thomas 2003 Flying and swimming animals cruise at a Strouhal number tuned for high power efficiency. Nature 425 707-711 10.1038/nature02000.
    • (2003) Nature , vol.425 , pp. 707-711
    • Taylor, G.K.1    Nudds, R.L.2    Thomas, A.L.R.3
  • 5
    • 0037230743 scopus 로고    scopus 로고
    • Forces on oscillating foils for propulsion and maneuvering
    • D.A. Read F.S. Hover M.S. Triantafyllou 2003 Forces on oscillating foils for propulsion and maneuvering. J. Fluids Struct. 17 163-183.
    • (2003) J. Fluids Struct. , vol.17 , pp. 163-183
    • Read, D.A.1    Hover, F.S.2    Triantafyllou, M.S.3
  • 6
    • 1142306116 scopus 로고    scopus 로고
    • Effect of angle of attack profiles in flapping foil propulsion
    • 10.1016/j.jfluidstructs.2003.10.003
    • F.S. Hover O. Haugsdal M.S. Triantafyllou 2004 Effect of angle of attack profiles in flapping foil propulsion. J. Fluids Struct. 19 37-47 10.1016/j.jfluidstructs.2003.10.003.
    • (2004) J. Fluids Struct. , vol.19 , pp. 37-47
    • Hover, F.S.1    Haugsdal, O.2    Triantafyllou, M.S.3
  • 7
    • 84983119302 scopus 로고    scopus 로고
    • Simulation of flow about flapping airfoils using finite element incompressible flow solver
    • Reno, Nevada
    • Ramamurti, R., Sandberg, W.: Simulation of flow about flapping airfoils using finite element incompressible flow solver. In: AIAA 37th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, pp. 253-260 (1999).
    • (1999) AIAA 37th Aerospace Sciences Meeting and Exhibit , pp. 253-260
    • Ramamurti, R.1    Sandberg, W.2
  • 8
    • 30044445962 scopus 로고    scopus 로고
    • The influence of the wake of a flapping wing on the production of aerodynamic forces
    • 10.1007/s10409-005-0064-4
    • J.H. Wu M. Sun 2005 The influence of the wake of a flapping wing on the production of aerodynamic forces. Acta Mech. Sinica 21 411-418 10.1007/s10409-005-0064-4.
    • (2005) Acta Mech. Sinica , vol.21 , pp. 411-418
    • Wu, J.H.1    Sun, M.2
  • 9
    • 59249101547 scopus 로고    scopus 로고
    • Near wake vortex dynamics of a hovering hawkmoth
    • H. Aono W. Shyy H. Liu 2009 Near wake vortex dynamics of a hovering hawkmoth Acta Mech. Sinica 25 (1) 25-36.
    • (2009) Acta Mech. Sinica , vol.25 , Issue.1 , pp. 25-36
    • Aono, H.1    Shyy, W.2    Liu, H.3
  • 10
    • 0038646169 scopus 로고    scopus 로고
    • A numerical study of the propulsive efficiency of a flapping hydrofoil
    • G. Pedro A. Suleman N. Djilali 2003 A numerical study of the propulsive efficiency of a flapping hydrofoil Int. J. Numer. Methods Fluids 42 493-526.
    • (2003) Int. J. Numer. Methods Fluids , vol.42 , pp. 493-526
    • Pedro, G.1    Suleman, A.2    Djilali, N.3
  • 11
    • 28844476537 scopus 로고    scopus 로고
    • Optimization of flapping airfoils for maximum thrust and propulsive efficiency
    • Reno, NV
    • Tuncer, I.H., Kaya, M.: Optimization of flapping airfoils for maximum thrust and propulsive efficiency. In: AIAA 41st Aerospace Sciences Meeting, Reno, NV, pp. 2329-2336 (2003).
    • (2003) AIAA 41st Aerospace Sciences Meeting , pp. 2329-2336
    • Tuncer, I.H.1    Kaya, M.2
  • 13
    • 0031206393 scopus 로고    scopus 로고
    • An arbitrary Lagrangian-Eulerian computing method for all flow speeds
    • C.W. Hirt A.A. Amsden J.L. Cook 1997 An arbitrary Lagrangian-Eulerian computing method for all flow speeds. J. Comput. Phys. 135 203-216.
    • (1997) J. Comput. Phys. , vol.135 , pp. 203-216
    • Hirt, C.W.1    Amsden, A.A.2    Cook, J.L.3
  • 14
    • 0001098774 scopus 로고    scopus 로고
    • A second-order time-accurate finite volume method for unsteady incompressible flow on hybrid unstructured grids
    • D. Kim H. Choi 2000 A second-order time-accurate finite volume method for unsteady incompressible flow on hybrid unstructured grids. J. Comput. Phys. 162 411-428.
    • (2000) J. Comput. Phys. , vol.162 , pp. 411-428
    • Kim, D.1    Choi, H.2
  • 18
    • 0025517092 scopus 로고
    • The structure of 2-dimensional separation
    • L.L. Pauley P. Moin W.C. Reynolds 1990 The structure of 2-dimensional separation. J. Fluid Mech. 220 397-411.
    • (1990) J. Fluid Mech. , vol.220 , pp. 397-411
    • Pauley, L.L.1    Moin, P.2    Reynolds, W.C.3
  • 20
    • 0038543178 scopus 로고    scopus 로고
    • Thrust generation caused by flapping airfoils in a biplane configuration
    • I.H. Tuncer M. Kaya 2003 Thrust generation caused by flapping airfoils in a biplane configuration. J. Aircr. 40 509-515.
    • (2003) J. Aircr. , vol.40 , pp. 509-515
    • Tuncer, I.H.1    Kaya, M.2
  • 21
    • 0033337119 scopus 로고    scopus 로고
    • Jet characteristics of a plunging airfoil
    • J.C.S. Lai M.F. Platzer 1999 Jet characteristics of a plunging airfoil. AIAA J. 37 1529-1537.
    • (1999) AIAA J. , vol.37 , pp. 1529-1537
    • Lai, J.C.S.1    Platzer, M.F.2
  • 22
    • 0042176897 scopus 로고    scopus 로고
    • Aerodynamics of small vehicles
    • 10.1146/annurev.fluid.35.101101.161102
    • T.J. Mueller J.D. DeLaurier 2003 Aerodynamics of small vehicles. Ann. Rev. Fluid Mech. 35 89-111 10.1146/annurev.fluid.35.101101.161102.
    • (2003) Ann. Rev. Fluid Mech. , vol.35 , pp. 89-111
    • Mueller, T.J.1    DeLaurier, J.D.2
  • 23
    • 10344220011 scopus 로고    scopus 로고
    • Leading-edge vortex lifts swifts
    • 10.1126/science.1104682
    • J.J. Videler E.J. Stamhuis G.D.E. Povel 2004 Leading-edge vortex lifts swifts. Science 306 1960-1962 10.1126/science.1104682.
    • (2004) Science , vol.306 , pp. 1960-1962
    • Videler, J.J.1    Stamhuis, E.J.2    Povel, G.D.E.3
  • 24
    • 84946657020 scopus 로고
    • Some new three level designs for the study of quantitative variables
    • G. Box D. Behnken 1960 Some new three level designs for the study of quantitative variables. Technometrics 2 455-475.
    • (1960) Technometrics , vol.2 , pp. 455-475
    • Box, G.1    Behnken, D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.