메뉴 건너뛰기




Volumn 222, Issue 1, 2008, Pages 63-80

Non-linear aeroelastic investigations of store(s)-induced limit cycle oscillations

Author keywords

Flutter; Limit cycle oscillations; Multiple store(s); Non linear aeroelasticity

Indexed keywords

FUEL TANKS; HOPF BIFURCATION; KINEMATICS; NONLINEAR ANALYSIS;

EID: 44449152621     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/09544100JAERO241     Document Type: Article
Times cited : (35)

References (40)
  • 3
    • 0242336478 scopus 로고    scopus 로고
    • Non-linear aeroelasticity
    • Dowell, E. H., Edwards, J., and Strganac, T. W. Non-linear aeroelasticity. J. Aircr., 2003, 40(5), 857-874.
    • (2003) J. Aircr , vol.40 , Issue.5 , pp. 857-874
    • Dowell, E.H.1    Edwards, J.2    Strganac, T.W.3
  • 4
    • 0000606320 scopus 로고    scopus 로고
    • Static and dynamic aeroelasticity of advanced aircraft wings carrying external stores
    • Gern, F. H. and Librescu, L. Static and dynamic aeroelasticity of advanced aircraft wings carrying external stores. AIAA J., 1998, 36(7), 1121-1129.
    • (1998) AIAA J , vol.36 , Issue.7 , pp. 1121-1129
    • Gern, F.H.1    Librescu, L.2
  • 5
    • 0032343549 scopus 로고    scopus 로고
    • Effect of externally mounted stores on flutter characteristics of advanced swept cantilevered aircraft wings
    • Gern, F. H. and Librescu, L. Effect of externally mounted stores on flutter characteristics of advanced swept cantilevered aircraft wings. Aerosp. Sci. Technol. J., 1998, 2(5), 321-333.
    • (1998) Aerosp. Sci. Technol. J , vol.2 , Issue.5 , pp. 321-333
    • Gern, F.H.1    Librescu, L.2
  • 6
    • 24644445990 scopus 로고    scopus 로고
    • Advances in the linear/non-linear control of aeroelastic structural systems
    • Librescu, L. and Marzocca, P. Advances in the linear/non-linear control of aeroelastic structural systems. Acta Mech., 2005, 178(3-4), 147-188.
    • (2005) Acta Mech , vol.178 , Issue.3-4 , pp. 147-188
    • Librescu, L.1    Marzocca, P.2
  • 7
    • 0036509548 scopus 로고    scopus 로고
    • Implications of cubic physical / aerodynamic non-linearities on the character of the flutter instability boundary
    • Librescu, L. and Marzocca, P. Implications of cubic physical / aerodynamic non-linearities on the character of the flutter instability boundary. Int. J. Non-linear Mech., 2003, 38, 173-199.
    • (2003) Int. J. Non-linear Mech , vol.38 , pp. 173-199
    • Librescu, L.1    Marzocca, P.2
  • 8
    • 0034272640 scopus 로고    scopus 로고
    • Limit cycle oscillation flight test results of a fighter with external stores
    • Denegri, C. Limit cycle oscillation flight test results of a fighter with external stores. J. Aircr., 2000, 37(5), 761-769.
    • (2000) J. Aircr , vol.37 , Issue.5 , pp. 761-769
    • Denegri, C.1
  • 10
    • 0034273920 scopus 로고    scopus 로고
    • Limit cycle oscillation characteristics of fighter aircraft
    • Bunton, R. and Denegri, C. Limit cycle oscillation characteristics of fighter aircraft. J. Aircr., 2000, 37(5), 916-918.
    • (2000) J. Aircr , vol.37 , Issue.5 , pp. 916-918
    • Bunton, R.1    Denegri, C.2
  • 11
    • 44449110100 scopus 로고    scopus 로고
    • Norton, W. J. Limit cycle oscillation and flight flutter testing. In Proceeding of the 21st Annual Symposium Society of Flight Test Engineers, Lancaster, CA, 1990, pp. 3.4.4-3.4.12.
    • Norton, W. J. Limit cycle oscillation and flight flutter testing. In Proceeding of the 21st Annual Symposium Society of Flight Test Engineers, Lancaster, CA, 1990, pp. 3.4.4-3.4.12.
  • 14
    • 0028757819 scopus 로고
    • Modal interactions in the forced vibration of a cantilever metallic plate
    • Oh, K., Nayfeh, A. H., and Mook, D. Modal interactions in the forced vibration of a cantilever metallic plate. Non-linear Stoch. Dyn., 1994, 192, 237-247.
    • (1994) Non-linear Stoch. Dyn , vol.192 , pp. 237-247
    • Oh, K.1    Nayfeh, A.H.2    Mook, D.3
  • 15
    • 0018152531 scopus 로고
    • Non-linear flexural-flexural-torsional dynamics of in extensional beam-I. Equations of motions
    • Crespo da Silva, M. R. M. and Glynn, C. Non-linear flexural-flexural-torsional dynamics of in extensional beam-I. Equations of motions. J. Struct. Mech., 1978, 6(4), 449-461.
    • (1978) J. Struct. Mech , vol.6 , Issue.4 , pp. 449-461
    • Crespo da Silva, M.R.M.1    Glynn, C.2
  • 16
    • 0003282964 scopus 로고
    • Three-dimensional non-linear vibrations of composite beams-I. Equations of motion
    • Pai, P. and Nayfeh, A. H. Three-dimensional non-linear vibrations of composite beams-I. Equations of motion, Nonlinear Dyn., 1990, 1, 477-502.
    • (1990) Nonlinear Dyn , vol.1 , pp. 477-502
    • Pai, P.1    Nayfeh, A.H.2
  • 20
    • 0036175844 scopus 로고    scopus 로고
    • Computational and experimental investigation of limit cycle oscillations of non-linear aeroelastic system
    • Sheta, E. F., Harrand, V. J., Thompson, D., and Strganac, T. Computational and experimental investigation of limit cycle oscillations of non-linear aeroelastic system. J. Aircr., 2002, 39(1), 133-141.
    • (2002) J. Aircr , vol.39 , Issue.1 , pp. 133-141
    • Sheta, E.F.1    Harrand, V.J.2    Thompson, D.3    Strganac, T.4
  • 21
    • 0034273845 scopus 로고    scopus 로고
    • Non-linear aeroelastic analysis of complete aircraft in subsonic flow
    • Patil, M. and Hodges, D. H. Non-linear aeroelastic analysis of complete aircraft in subsonic flow. J. Aircr., 2000, 37(5), 753-760.
    • (2000) J. Aircr , vol.37 , Issue.5 , pp. 753-760
    • Patil, M.1    Hodges, D.H.2
  • 23
    • 0035421036 scopus 로고    scopus 로고
    • Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings
    • Tang, D. and Dowell, E. H. Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings. AIAA J., 2001, 39(8), 1430-1441.
    • (2001) AIAA J , vol.39 , Issue.8 , pp. 1430-1441
    • Tang, D.1    Dowell, E.H.2
  • 24
    • 0004090333 scopus 로고
    • Non-linear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades
    • Report TN D-7818, NASA
    • Dowell, E. H. and Hodges, D. Non-linear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades. Report TN D-7818, NASA, 1974.
    • (1974)
    • Dowell, E.H.1    Hodges, D.2
  • 25
    • 0017452683 scopus 로고    scopus 로고
    • An experimental-theoretical correlation study of nonlinear bending and torsion deformations of a cantilever beam
    • Dowell, E. H., Traybar, J., and Hodges, D. H. An experimental-theoretical correlation study of nonlinear bending and torsion deformations of a cantilever beam. J. Sound Vibr., 1997, 50, 533-544.
    • (1997) J. Sound Vibr , vol.50 , pp. 533-544
    • Dowell, E.H.1    Traybar, J.2    Hodges, D.H.3
  • 26
    • 0003213977 scopus 로고
    • Non-linear effects in the static and dynamic behaviour of beams and rotor blades
    • Hodges, D. H., Crespo da Silva, M., and Peters, D. Non-linear effects in the static and dynamic behaviour of beams and rotor blades. Vertica, 1988, 12(3), 243-256.
    • (1988) Vertica , vol.12 , Issue.3 , pp. 243-256
    • Hodges, D.H.1    Crespo da Silva, M.2    Peters, D.3
  • 27
    • 0042011109 scopus 로고    scopus 로고
    • Kim, K. and Strganac, T. W. Non-linear responses of a cantilever wing with an external store. In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Norfolk, VA, 7-10 April 2003, AIAA paper 2003-1708
    • Kim, K. and Strganac, T. W. Non-linear responses of a cantilever wing with an external store. In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Norfolk, VA, 7-10 April 2003, AIAA paper 2003-1708
  • 28
    • 7544238048 scopus 로고    scopus 로고
    • Studies of store-induced limit cycle oscillations using a model with full system non-linearities
    • Beran, P. S., Strganac, T. W., Kim, K., and Nichkawde, C. Studies of store-induced limit cycle oscillations using a model with full system non-linearities. Non-linear Dyn., 2004, 37, 323-339.
    • (2004) Non-linear Dyn , vol.37 , pp. 323-339
    • Beran, P.S.1    Strganac, T.W.2    Kim, K.3    Nichkawde, C.4
  • 29
    • 17444380082 scopus 로고    scopus 로고
    • Non-linear analysis of store-induced limit cycle oscillations
    • Thompson, D. and Strganac, T. W. Non-linear analysis of store-induced limit cycle oscillations. Non-linear Dyn., 2005, 39, 159-178.
    • (2005) Non-linear Dyn , vol.39 , pp. 159-178
    • Thompson, D.1    Strganac, T.W.2
  • 30
    • 44449179854 scopus 로고    scopus 로고
    • Modeling the LCO of a delta wing with an external store using a high fidelity structural model
    • AIAA paper 2005-1913
    • Attar, P. J., Dowell, E. H., and Tang, D. Modeling the LCO of a delta wing with an external store using a high fidelity structural model. AIAA paper 2005-1913, 2005.
    • (2005)
    • Attar, P.J.1    Dowell, E.H.2    Tang, D.3
  • 31
    • 26644464848 scopus 로고    scopus 로고
    • Dynamic aeroelastic instabilities of an aircraft wing with underwing store in transonic regime
    • Byreddy, C., Grandhi, R. V., and Beran, P. Dynamic aeroelastic instabilities of an aircraft wing with underwing store in transonic regime. J. Aerosp. Eng., 2005, 18(4), 206-214.
    • (2005) J. Aerosp. Eng , vol.18 , Issue.4 , pp. 206-214
    • Byreddy, C.1    Grandhi, R.V.2    Beran, P.3
  • 32
    • 85086614023 scopus 로고    scopus 로고
    • Influence of tip store mass location on wing limit cycle oscillation
    • Norfolk, VA, 7-10 April, Reston, VA, AIAA paper 2003-1731 American Institute of Aeronautics and Astronautics, Inc
    • Khot, N. S., Beran, P. S., Zweber, J. V., and Eastep, F. E. Influence of tip store mass location on wing limit cycle oscillation. In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Norfolk, VA, 7-10 April 2003, Reston, VA, AIAA paper 2003-1731 (American Institute of Aeronautics and Astronautics, Inc.).
    • (2003) 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
    • Khot, N.S.1    Beran, P.S.2    Zweber, J.V.3    Eastep, F.E.4
  • 33
    • 0036072719 scopus 로고    scopus 로고
    • Influence of external store aerodynamics on flutter/LCO of a fighter aircraft
    • Denver, CO, 22-25 April, Reston, VA, AIAA paper 2002-1410 American Institute of Aeronautics and Astronautics, Inc
    • Chen, P. C., Sulaeman, E., Liu, D. D., and Denegri, C. M. Influence of external store aerodynamics on flutter/LCO of a fighter aircraft. In 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Denver, CO, 22-25 April 2002, Reston, VA, AIAA paper 2002-1410 (American Institute of Aeronautics and Astronautics, Inc.).
    • (2002) 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
    • Chen, P.C.1    Sulaeman, E.2    Liu, D.D.3    Denegri, C.M.4
  • 34
    • 10944233712 scopus 로고    scopus 로고
    • Numerical analysis of store-induced limit-cycle oscillation
    • Beran, P. S., Khot, N. S., Eastep, F. E., Snyder, R. D., and Zweber, J. V. Numerical analysis of store-induced limit-cycle oscillation. J. Aircr., 2004, 41(6), 1315-1326.
    • (2004) J. Aircr , vol.41 , Issue.6 , pp. 1315-1326
    • Beran, P.S.1    Khot, N.S.2    Eastep, F.E.3    Snyder, R.D.4    Zweber, J.V.5
  • 35
    • 12744274620 scopus 로고    scopus 로고
    • Non-linear aeroelastic computations of a wing/pylon/finnedstore using parallel computing
    • Kim, D. H., Park, Y. M., Lee, I., and Kuon, O. J. Non-linear aeroelastic computations of a wing/pylon/finnedstore using parallel computing. AIAA J., 2005, 43(1), 53-62
    • (2005) AIAA J , vol.43 , Issue.1 , pp. 53-62
    • Kim, D.H.1    Park, Y.M.2    Lee, I.3    Kuon, O.J.4
  • 39
    • 0030172890 scopus 로고    scopus 로고
    • Aeroelastic analysis of a flexible airfoil with a freeplay non-linearity
    • Kim, S. H. and Lee, I. Aeroelastic analysis of a flexible airfoil with a freeplay non-linearity. J. Sound Vibr., 1996, 194, 823-846.
    • (1996) J. Sound Vibr , vol.194 , pp. 823-846
    • Kim, S.H.1    Lee, I.2
  • 40
    • 0034316194 scopus 로고    scopus 로고
    • Identification and control of limit cycle oscillations in aeroelastic system
    • Strganac, T., Ko, J., and Thompson, D. Identification and control of limit cycle oscillations in aeroelastic system. J. Guid. Control Dyn., 2000, 23(6), 1127-1133.
    • (2000) J. Guid. Control Dyn , vol.23 , Issue.6 , pp. 1127-1133
    • Strganac, T.1    Ko, J.2    Thompson, D.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.