-
1
-
-
0025888833
-
Sixteen degrees of freedom rectangular plate element
-
Bismarck-Nasr MN (1991a), Sixteen degrees of freedom rectangular plate element, Int J of Comput Struct, 40(4), 1059-1060.
-
(1991)
Int J of Comput Struct
, vol.40
, Issue.4
, pp. 1059-1060
-
-
Bismarck-Nasr, M.N.1
-
2
-
-
0026186354
-
Enhancement of the accuracy in direct integration dynamic response problems
-
Bismarck-Nasr MN and de Oliveira AM (1991b), Enhancement of the accuracy in direct integration dynamic response problems, Earthquake Eng Struct Dyn, 20(7), 699-703.
-
(1991)
Earthquake Eng Struct Dyn
, vol.20
, Issue.7
, pp. 699-703
-
-
Bismarck-Nasr, M.N.1
De Oliveira, A.M.2
-
3
-
-
0026868056
-
Coalescence of aeroelastic modes in flutter analysis
-
Bismarck-Nasr MN (1992a), Coalescence of aeroelastic modes in flutter analysis, JAircraft, 29(3), 505-507.
-
(1992)
Jaircraft
, vol.29
, Issue.3
, pp. 505-507
-
-
Bismarck-Nasr, M.N.1
-
4
-
-
84951738669
-
Finite element analysis of aeroelasticity of plates and shells
-
Bismarck-Nasr MN (1992b), Finite element analysis of aeroelasticity of plates and shells, ApplMech Rev, 45(12), 461-482.
-
(1992)
Applmech Rev
, vol.45
, Issue.12
, pp. 461-482
-
-
Bismarck-Nasr, M.N.1
-
5
-
-
3643087271
-
Vibrations of thin cylindrically curved panels
-
Sao Paulo, Brazil
-
Bismarck-Nasr MN (1993-a), Vibrations of thin cylindrically curved panels, Proc of 3rd Pan American Congress of Appl Mech, PACAM III, Sao Paulo, Brazil, 696-699.
-
(1993)
Proc of 3Rd Pan American Congress of Appl Mech, PACAM III
, pp. 696-699
-
-
Bismarck-Nasr, M.N.1
-
6
-
-
0027626729
-
Supersonic panel flutter analysis of shallow shells
-
Bismarck-Nasr MN (1993b), Supersonic panel flutter analysis of shallow shells, AIAA J, 31(7), 1349-1351.
-
(1993)
AIAA J
, vol.31
, Issue.7
, pp. 1349-1351
-
-
Bismarck-Nasr, M.N.1
-
7
-
-
85002667536
-
Analysis of cylindrically curved panels based on a two field variable variational principle
-
Bismarck-Nasr MN (1993-c), Analysis of cylindrically curved panels based on a two field variable variational principle, Appl Mech Rev, 46(11), Pt2, 571-578.
-
(1993)
Appl Mech Rev
, vol.46
, Issue.11
, pp. 571-578
-
-
Bismarck-Nasr, M.N.1
-
8
-
-
0028429523
-
Buckling analysis of cylindrically curved panels based on a two field variational principle
-
Bismarck-Nasr MN (1994a), Buckling analysis of cylindrically curved panels based on a two field variational principle, Int J Comput Struct, 51(4), 453-457.
-
(1994)
Int J Comput Struct
, vol.51
, Issue.4
, pp. 453-457
-
-
Bismarck-Nasr, M.N.1
-
9
-
-
0028466123
-
Direct solution of the aeroelastic stability equations
-
Bismarck-Nasr MN (1994b), Direct solution of the aeroelastic stability equations, J Aircraft, 31(4), 979-981.
-
(1994)
J Aircraft
, vol.31
, Issue.4
, pp. 979-981
-
-
Bismarck-Nasr, M.N.1
-
10
-
-
0029255835
-
Dynamic stability of shallow shells subjected to follower forces
-
Bismarck-Nasr MN (1995a), Dynamic stability of shallow shells subjected to follower forces, AIAA J, 33(2), 355-360.
-
(1995)
AIAA J
, vol.33
, Issue.2
, pp. 355-360
-
-
Bismarck-Nasr, M.N.1
-
11
-
-
5544243308
-
Vibration of laminated doubly curved shallow shells
-
PACAM IV, Buenes Aires, Argentina
-
Bismarck-Nasr MN and Silva DAH (1995b), Vibration of laminated doubly curved shallow shells, Proc of 4th Pan American Congress of ApplMech, PACAM IV, Buenes Aires, Argentina, Vol 1, 337-342.
-
(1995)
Proc of 4Th Pan American Congress of Applmech
, vol.1
, pp. 337-342
-
-
Bismarck-Nasr, M.N.1
Silva, D.2
-
13
-
-
85007691239
-
Nonlinear oscillations of a fluttering plate
-
Dowell EH (1966), Nonlinear oscillations of a fluttering plate, AIAA J, 4(7), 1267-1275.
-
(1966)
AIAA J
, vol.4
, Issue.7
, pp. 1267-1275
-
-
Dowell, E.H.1
-
14
-
-
85007669250
-
Nonlinear oscillations of a fluttering plate II
-
Dowell EH (1967), Nonlinear oscillations of a fluttering plate II, AIAA J, 5(10), 1856-1862.
-
(1967)
AIAA J
, vol.5
, Issue.10
, pp. 1856-1862
-
-
Dowell, E.H.1
-
15
-
-
85007687633
-
Nonlinear flutter of curved plates
-
Dowell EH (1969), Nonlinear flutter of curved plates, AIAA J, 7(3), 424-431.
-
(1969)
AIAA J
, vol.7
, Issue.3
, pp. 424-431
-
-
Dowell, E.H.1
-
16
-
-
0014735720
-
Nonlinear flutter of curved plates II
-
Dowell EH (1970), Nonlinear flutter of curved plates II, AIAA J, 8(2) 259-261.
-
(1970)
AIAA J
, vol.8
, Issue.2
, pp. 259-261
-
-
Dowell, E.H.1
-
19
-
-
5544223833
-
Analysis of nonlinear panel flutter and response under random excitation or nonlinear aerodynamic loadings
-
Denver CO, April 22-24
-
Eastep FE and McIntosh SC (1970), Analysis of nonlinear panel flutter and response under random excitation or nonlinear aerodynamic loadings, AIAA/ASME II Structures, Structural Dyn, and Mat Conf Denver CO, April 22-24, pp 36-47.
-
(1970)
AIAA/ASME II Structures, Structural Dyn, and Mat Conf
, pp. 36-47
-
-
Eastep, F.E.1
McIntosh, S.C.2
-
22
-
-
0011405046
-
Two-dimensional panel flutter
-
Fung YC (1958), Two-dimensional panel flutter, J Aero/Space Sci, 25(3) 145-159.
-
(1958)
J Aero/Space Sci
, vol.25
, Issue.3
, pp. 145-159
-
-
Fung, Y.C.1
-
24
-
-
0026104722
-
Finite element method for large amplitude two-dimensional panel flutter at hypersonic speeds
-
Gray Jr CE, Mei C, and Shore CP (1991), Finite element method for large amplitude two-dimensional panel flutter at hypersonic speeds, AIAA J, 29(2) 290-298.
-
(1991)
AIAA J
, vol.29
, Issue.2
, pp. 290-298
-
-
Gray, C.E.1
Mei, C.2
Shore, C.P.3
-
25
-
-
0027608487
-
Large amplitude finite element flutter analysis of composite panels in hypersonic flow
-
Gray Jr CE and Mei C (1993), Large amplitude finite element flutter analysis of composite panels in hypersonic flow, AIAA J, 31(6) 1090-1099.
-
(1993)
AIAA J
, vol.31
, Issue.6
, pp. 1090-1099
-
-
Gray, C.E.1
Mei, C.2
-
26
-
-
0020841735
-
Nonlinear panel flutter using high order triangular finite elements
-
Han AD and Yang TY (1983), Nonlinear panel flutter using high order triangular finite elements, AIAA J, 21(10) 1453-1461.
-
(1983)
AIAA J
, vol.21
, Issue.10
, pp. 1453-1461
-
-
Han, A.D.1
Yang, T.Y.2
-
27
-
-
0005018849
-
Physical nature of panel flutter
-
Jordan PF (1956), Physical nature of panel flutter, Aero Digest, 34-38.
-
(1956)
Aero Digest
, pp. 34-38
-
-
Jordan, P.F.1
-
28
-
-
0010122571
-
Flutter of simply-supported rectangular panels in a supersonic flow; two dimensional panel flutter I, simply supported panel II, clamped panel
-
Kobayashi S (1962), Flutter of simply-supported rectangular panels in a supersonic flow; two dimensional panel flutter I, simply supported panel II, clamped panel, Trans Japan Soc of Aeronaut and Space Sci, 5, 79118.
-
(1962)
Trans Japan Soc of Aeronaut and Space Sci
, vol.5
, pp. 79118
-
-
Kobayashi, S.1
-
29
-
-
0015434615
-
Perturbation and harmonic balance methods for nonlinear panel flutter
-
Kuo CC, Morino L and Dugundgi J (1972), Perturbation and harmonic balance methods for nonlinear panel flutter, AIAA J, 10(11) 1479-1484.
-
(1972)
AIAA J
, vol.10
, Issue.11
, pp. 1479-1484
-
-
Kuo, C.C.1
Morino, L.2
Dugundgi, J.3
-
30
-
-
0002441941
-
Aeroelastic stability of orthotropic heterogeneous thin panels in the vicinity of the flutter critical boundary
-
Librescu L (1965), Aeroelastic stability of orthotropic heterogeneous thin panels in the vicinity of the flutter critical boundary, J de mécanique, 4(1) 51-76.
-
(1965)
J De mécanique
, vol.4
, Issue.1
, pp. 51-76
-
-
Librescu, L.1
-
33
-
-
0017520420
-
A finite element approach for nonlinear panel flutter
-
Mei C (1977), A finite element approach for nonlinear panel flutter, AIAA J, 15(8) 1107-1110.
-
(1977)
AIAA J
, vol.15
, Issue.8
, pp. 1107-1110
-
-
Mei, C.1
-
34
-
-
0017680553
-
Nonlinear panel flutter-A finite element approach
-
T Belytschko and TL Geers (Eds), AMR, American Society of Mechanical Engineers
-
Mei C and Weidman DJ (1977), Nonlinear panel flutter-A finite element approach, Computational methods for fluid-structure interaction problems, T Belytschko and TL Geers (Eds), AMR-Vol 26, American Society of Mechanical Engineers, 139-165.
-
(1977)
Computational Methods for Fluid-Structure Interaction Problems
, vol.26
, pp. 139-165
-
-
Mei, C.1
Weidman, D.J.2
-
35
-
-
0039523950
-
Finite elements analysis of large amplitude supersonic flutter of panels
-
(Shangai, China), Gordon and Breach, New York
-
Mei C and Wang HC (1982), Finite elements analysis of large amplitude supersonic flutter of panels, Proc of Int Conf on FEMs (Shangai, China), Gordon and Breach, New York, 944-951.
-
(1982)
Proc of Int Conf on Fems
, pp. 944-951
-
-
Mei, C.1
Wang, H.C.2
-
37
-
-
85007710224
-
Perturbation method for treating nonlinear panel lutter problems
-
Morino L (1969), Perturbation method for treating nonlinear panel lutter problems, AIAA J, 7(3) 405-411.
-
(1969)
AIAA J
, vol.7
, Issue.3
, pp. 405-411
-
-
Morino, L.1
-
38
-
-
0028993516
-
Optimal design of composite lifting surface for flutter suppression with piezoelectric actuators
-
Nam C and Kim Y (1995), Optimal design of composite lifting surface for flutter suppression with piezoelectric actuators, AIAA J, 33(10) 1897-1904.
-
(1995)
AIAA J
, vol.33
, Issue.10
, pp. 1897-1904
-
-
Nam, C.1
Kim, Y.2
-
40
-
-
85007716519
-
Stability criterion for panel flutter via the second method of Liupanov
-
Parks PC (1966), Stability criterion for panel flutter via the second method of Liupanov, AIAA J, 4(1) 175-178.
-
(1966)
AIAA J
, vol.4
, Issue.1
, pp. 175-178
-
-
Parks, P.C.1
-
41
-
-
0027609110
-
Supersonic flutter analysis of composite plates and shells
-
Pidaparti RMV and Yang HTY (1993), Supersonic flutter analysis of composite plates and shells, AIAA J, 31(6) 1109-1117.
-
(1993)
AIAA J
, vol.31
, Issue.6
, pp. 1109-1117
-
-
Pidaparti, R.1
Yang, H.2
-
42
-
-
0005451593
-
Large amplitude supersonic flutter of panels with ends elastically restrained against rotation
-
Rao KS and Rao GV (1980), Large amplitude supersonic flutter of panels with ends elastically restrained against rotation, Comput Struct, 11(3) 197-201.
-
(1980)
Comput Struct
, vol.11
, Issue.3
, pp. 197-201
-
-
Rao, K.S.1
Rao, G.V.2
-
43
-
-
0028195864
-
Panel flutter suppression using adaptive material actuators
-
Scott RC and Weisshaar TA (1994), Panel flutter suppression using adaptive material actuators, J Aircraft, 31(1) 213-222.
-
(1994)
J Aircraft
, vol.31
, Issue.1
, pp. 213-222
-
-
Scott, R.C.1
Weisshaar, T.A.2
-
44
-
-
0027334457
-
Finite element nonlinear flutter with arbitrary temperatures in supersonic flow
-
Xue DY and Mei C (1993), Finite element nonlinear flutter with arbitrary temperatures in supersonic flow, AIAA J, 31(1) 154-162.
-
(1993)
AIAA J
, vol.31
, Issue.1
, pp. 154-162
-
-
Xue, D.Y.1
Mei, C.2
-
46
-
-
0028519470
-
Finite element time domain -Model formulation for nonlinear flutter of composite panels
-
Zhou RC, Xue DY, and Mei C (1994), Finite element time domain -Model formulation for nonlinear flutter of composite panels, AIAA J, 32(10) 2044-2059.
-
(1994)
AIAA J
, vol.32
, Issue.10
, pp. 2044-2059
-
-
Zhou, R.C.1
Xue, D.Y.2
Mei, C.3
-
47
-
-
0029167465
-
Suppresion of nonlinear panel flutter with piezoelectric actuators using finite element method
-
Zhou RC, Lai Z, Xue DY, Huang JK and Mei C (1995), Suppresion of nonlinear panel flutter with piezoelectric actuators using finite element method, AIAA J, 33(6) 1098-1105.
-
(1995)
AIAA J
, vol.33
, Issue.6
, pp. 1098-1105
-
-
Zhou, R.C.1
Lai, Z.2
Xue, D.Y.3
Huang, J.K.4
Mei, C.5
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