-
1
-
-
0028378081
-
Minimum-weight design of a stiffened panel via PANDA2 and evaluation of the optimized panel via STAGS
-
D. Bushnell and W. D. Bushnell, Minimum-weight design of a stiffened panel via PANDA2 and evaluation of the optimized panel via STAGS. Comput. Struct. 50, 569-602 (1994).
-
(1994)
Comput. Struct.
, vol.50
, pp. 569-602
-
-
Bushnell, D.1
Bushnell, W.D.2
-
2
-
-
11544313883
-
Optimization of laminate stacking sequence for buckling load maximization by genetic algorithm
-
AIAA paper 92-2314-CP
-
R. Le Riche and R. T. Haftka, Optimization of laminate stacking sequence for buckling load maximization by genetic algorithm. AIAA paper 92-2314-CP, Proc. 33rd AIAA Structures, Structural Dynamics, and Materials Conf., Part 5, pp. 2564-2575.
-
Proc. 33rd AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.5 PART
, pp. 2564-2575
-
-
Le Riche, R.1
Haftka, R.T.2
-
3
-
-
0012836995
-
Optimization of composite plates for buckling by simulated annealing
-
AIAA paper 92-2313-CP
-
M. Lombardi, R. T. Haftka and C. Cinquini, Optimization of composite plates for buckling by simulated annealing. AIAA paper 92-2313-CP, Proc. 33rd AIAA Structures, Structural Dynamics and Materials Conf., Part 5, pp. 2552-2563 (1992).
-
(1992)
Proc. 33rd AIAA Structures, Structural Dynamics and Materials Conf.
, Issue.5 PART
, pp. 2552-2563
-
-
Lombardi, M.1
Haftka, R.T.2
Cinquini, C.3
-
4
-
-
0041636998
-
Stacking sequence optimization of simply supported laminates with stability and strain constraints
-
AIAA paper 92-2310-CP
-
S. Nagendra, R. T. Haftka and Z. Gürdal, Stacking sequence optimization of simply supported laminates with stability and strain constraints. AIAA paper 92-2310-CP, Proc. 33rd AIAA Structures, Structural Dynamics, and Materials Conf., Part 5, pp. 2526-2535 (1992).
-
(1992)
Proc. 33rd AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.5 PART
, pp. 2526-2535
-
-
Nagendra, S.1
Haftka, R.T.2
Gürdal, Z.3
-
5
-
-
0026835516
-
Stacking sequence optimization for buckling of laminated plates by integer programming
-
AIAA paper 91-0970-CP
-
R. T. Haftka and J. L. Walsh, Stacking sequence optimization for buckling of laminated plates by integer programming. AIAA paper 91-0970-CP, Proc. 32nd AIAA Structures, Structural Dynamics, and Materials Conf., Part 1, pp. 267-274 (1991).
-
(1991)
Proc. 32nd AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.1 PART
, pp. 267-274
-
-
Haftka, R.T.1
Walsh, J.L.2
-
6
-
-
0027607686
-
Postbuckling of geometrically imperfect shear-deformable flat panels under combined thermal and compressive edge loadings
-
L. Librescu and M. A. Souza, Postbuckling of geometrically imperfect shear-deformable flat panels under combined thermal and compressive edge loadings. J. Appl. Mech. 60, 526-534 (1993).
-
(1993)
J. Appl. Mech.
, vol.60
, pp. 526-534
-
-
Librescu, L.1
Souza, M.A.2
-
7
-
-
84914919973
-
Structural analysis and sizing of stiffened, metal matrix composite panels for hypersonic vehicles
-
1-4 December, Orlando, FL
-
C. Collier, Structural analysis and sizing of stiffened, metal matrix composite panels for hypersonic vehicles. In: Proc. AIAA Fourth Int. Aerospace Planes Conf., 1-4 December, Orlando, FL (1992).
-
(1992)
Proc. AIAA Fourth Int. Aerospace Planes Conf.
-
-
Collier, C.1
-
8
-
-
0042138022
-
Combined compressive and shear buckling analysis of hypersonic aircraft sandwich panels
-
AIAA paper 92-2487-CP
-
W. L. Ko and R. H. Jackson, Combined compressive and shear buckling analysis of hypersonic aircraft sandwich panels. AIAA paper 92-2487-CP, Proc. 33rd AIAA Structures, Structural Dynamics, and Materials Conf., Part 5, pp. 3198-3225 (1992).
-
(1992)
Proc. 33rd AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.5 PART
, pp. 3198-3225
-
-
Ko, W.L.1
Jackson, R.H.2
-
9
-
-
0042138010
-
Thermally-induced, geometrically nonlinear response of symmetrically laminated composite plates
-
AIAA paper 92-2539-CP
-
C. A. Meyers and M. W. Hyer, Thermally-induced, geometrically nonlinear response of symmetrically laminated composite plates. AIAA paper 92-2539-CP, Proc. 33rd AIAA Structure, Structural Dynamics, and Materials Conf., Part 2, pp. 1027-1037 (1992).
-
(1992)
Proc. 33rd AIAA Structure, Structural Dynamics, and Materials Conf.
, Issue.2 PART
, pp. 1027-1037
-
-
Meyers, C.A.1
Hyer, M.W.2
-
10
-
-
0041415619
-
Thermomechanical buckling and postbuckling of multilayered composite panels
-
AIAA paper 92-2541-CP
-
A. K. Noor, J. H. Starnes Jr and J. M. Peters, Thermomechanical buckling and postbuckling of multilayered composite panels. AIAA paper 92-2541-CP, Proc. 33rd AIAA Structures, Structural Dynamics, and Materials Conf., Part 2, pp. 1052-1068 (1992).
-
(1992)
Proc. 33rd AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.2 PART
, pp. 1052-1068
-
-
Noor, A.K.1
Starnes J.H., Jr.2
Peters, J.M.3
-
11
-
-
0042638956
-
Thermal buckling of anisotropic laminated cylindrically curved panels
-
AIAA paper 91-0915-CP
-
K. Chandrashekhara, Thermal buckling of anisotropic laminated cylindrically curved panels. AIAA paper 91-0915-CP, Proc. 32nd AIAA Structures, Structural Dynamics, and Materials Conf., Part 2, pp. 933-937 (1991).
-
(1991)
Proc. 32nd AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.2 PART
, pp. 933-937
-
-
Chandrashekhara, K.1
-
12
-
-
0040023908
-
Inclusion of transverse shear deformation in exact buckling and vibration analysis of composite plate assemblies
-
AIAA paper 92-2287-CP
-
M. S. Anderson and D. Kennedy, Inclusion of transverse shear deformation in exact buckling and vibration analysis of composite plate assemblies. AIAA paper 92-2287-CP, Proc. 33nd AIAA Structures, Structural Dynamics, and Materials Conf., Part 1, pp. 283-291 (1992).
-
(1992)
Proc. 33nd AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.1 PART
, pp. 283-291
-
-
Anderson, M.S.1
Kennedy, D.2
-
13
-
-
0025460866
-
Pre- and postbuckling finite element analysis of curved composite and sandwich panels
-
J.-P. Jeusette and G. Laschet, Pre- and postbuckling finite element analysis of curved composite and sandwich panels. AIAA J. 28, 1233-1239 (1990).
-
(1990)
AIAA J.
, vol.28
, pp. 1233-1239
-
-
Jeusette, J.-P.1
Laschet, G.2
-
14
-
-
0042138021
-
Postbuckling behavior of shear deformable flat panels under the complex action of thermal and in-plane mechanical loadings
-
AIAA paper 91-0913-CP
-
L. Librescu and M. A. Souza, Postbuckling behavior of shear deformable flat panels under the complex action of thermal and in-plane mechanical loadings. AIAA paper 91-0913-CP, Proc. 32nd AIAA Structures, Structural Dynamics, and Materials Conf., Part 2, pp. 917-925 (1991).
-
(1991)
Proc. 32nd AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.2 PART
, pp. 917-925
-
-
Librescu, L.1
Souza, M.A.2
-
15
-
-
0026082358
-
A geometrically nonlinear theory of transversely isotropic laminated composite plates and its use in the post-buckling analysis
-
L. Librescu and M. Stein, A geometrically nonlinear theory of transversely isotropic laminated composite plates and its use in the post-buckling analysis. Thin-Walled Struct., 11, 177-01 (1991).
-
(1991)
Thin-walled Struct.
, vol.11
, pp. 177-201
-
-
Librescu, L.1
Stein, M.2
-
16
-
-
0001186392
-
Effects of geometric imperfections on vibration of compressed shear deformable laminated composite curved panels
-
L. Librescu and M.-Y. Chang, Effects of geometric imperfections on vibration of compressed shear deformable laminated composite curved panels. Acta Mech. 96, 203-224 (1993).
-
(1993)
Acta Mech.
, vol.96
, pp. 203-224
-
-
Librescu, L.1
Chang, M.-Y.2
-
17
-
-
0027287036
-
Thermomechanical postbuckling analysis of laminated composite shells
-
AIAA paper 93-1337-CP
-
R. C. Averill and J. N. Reedy, Thermomechanical postbuckling analysis of laminated composite shells. AIAA paper 93-1337-CP, Proc. 34th AIAA Structures, Structural Dynamics, and Materials Conf., Part 1, pp. 351-360 (1993).
-
(1993)
Proc. 34th AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.1 PART
, pp. 351-360
-
-
Averill, R.C.1
Reedy, J.N.2
-
18
-
-
0027149243
-
Buckling of moderately thick, laminated cylindrical shells under torsion
-
AIAA paper 93-1334-CP
-
A. Tabiei and G. J. Simitses, Buckling of moderately thick, laminated cylindrical shells under torsion. AIAA paper 93-1334-CP, Proc. 34th AIAA Structures, Structural Dynamics, and Materials Conf., Part 1, pp. 315-325 (1993).
-
(1993)
Proc. 34th AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.1 PART
, pp. 315-325
-
-
Tabiei, A.1
Simitses, G.J.2
-
19
-
-
0042138025
-
Buckling behavior of long symmetrically laminated plates subjected to compresion, shear, and inplane bending loads
-
AIAA paper 92-2286-CP
-
M. P. Nemeth, Buckling behavior of long symmetrically laminated plates subjected to compresion, shear, and inplane bending loads. AIAA paper 92-2286-CP, Proc. 33rd AIAA Structures, Structural Dynamics, and Materials Conf., Part 2, pp. 274-282 (1992).
-
(1992)
Proc. 33rd AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.2 PART
, pp. 274-282
-
-
Nemeth, M.P.1
-
20
-
-
0042638959
-
Instability in a cylindrical panel subjected to normal pressure
-
AIAA paper 92-2234-CP
-
S. T. Dennis, B. A. Horban and A. N. Palazotto, Instability in a cylindrical panel subjected to normal pressure. AIAA paper 92-2234-CP, Proc. 33rd AIAA Structure, Structural Dynamics, and Materials Conf., Part 1, pp. 100-108 (1992).
-
(1992)
Proc. 33rd AIAA Structure, Structural Dynamics, and Materials Conf.
, Issue.1 PART
, pp. 100-108
-
-
Dennis, S.T.1
Horban, B.A.2
Palazotto, A.N.3
-
21
-
-
0042638957
-
Buckling, postbuckling, and failure behavior of composite-stiffened panels under axial compression
-
AIAA paper 92-2285-CP
-
S. Fan, B. Kroplin and B. Geier, Buckling, postbuckling, and failure behavior of composite-stiffened panels under axial compression. AIAA paper 92-2285-CP, Proc. 33rd AIAA Structures, Structural Dynamic, and Materials Conf., Part 1, pp. 264-273 (1992).
-
(1992)
Proc. 33rd AIAA Structures, Structural Dynamic, and Materials Conf.
, Issue.1 PART
, pp. 264-273
-
-
Fan, S.1
Kroplin, B.2
Geier, B.3
-
22
-
-
0025067310
-
Durability of stiffened composite panels under repeated buckling
-
T. Weller and J. Singer, Durability of stiffened composite panels under repeated buckling. Int. J. Solids Struct. 26, 1037-1069 (1990).
-
(1990)
Int. J. Solids Struct.
, vol.26
, pp. 1037-1069
-
-
Weller, T.1
Singer, J.2
-
23
-
-
0043139934
-
MacPASCO: A Macintosh-based interactive graphic preprocessor for structural analysis and sizing
-
AIAA paper 91-1208-CP
-
S. H. Lucas and R. C. Davis, MacPASCO: a Macintosh-based interactive graphic preprocessor for structural analysis and sizing. AIAA paper 91-1208-CP, Proc. 32nd AIAA Structures, Structural Dynamic, and Materials Conf., Part 1, pp. 612-626 (1991).
-
(1991)
Proc. 32nd AIAA Structures, Structural Dynamic, and Materials Conf.
, Issue.1 PART
, pp. 612-626
-
-
Lucas, S.H.1
Davis, R.C.2
-
24
-
-
0043139933
-
Buckling of imperfect, anisotropic, ring-stiffened cylinders under combined loads
-
AIAA paper 92-2232-CP
-
R. P. Ley, E. R. Johnson and Z. Gürdal, Buckling of imperfect, anisotropic, ring-stiffened cylinders under combined loads. AIAA paper 92-2232-CP, Proc 33rd AIAA Structures, Structural Dynamics, and Materials Conf., Part 1, pp. 86-94. AIAA J. (in press).
-
Proc 33rd AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.1 PART
, pp. 86-94
-
-
Ley, R.P.1
Johnson, E.R.2
Gürdal, Z.3
-
25
-
-
85029984961
-
-
in press
-
R. P. Ley, E. R. Johnson and Z. Gürdal, Buckling of imperfect, anisotropic, ring-stiffened cylinders under combined loads. AIAA paper 92-2232-CP, Proc 33rd AIAA Structures, Structural Dynamics, and Materials Conf., Part 1, pp. 86-94. AIAA J. (in press).
-
AIAA J.
-
-
-
26
-
-
0027266181
-
Optimal design of imperfect anisotropic, ring-stiffened cylinders under combined loads
-
AIAA paper 93-1526-CP
-
R. P. Ley, Z. Gürdal and E. R. Johnson, Optimal design of imperfect anisotropic, ring-stiffened cylinders under combined loads. AIAA paper 93-1526-CP. Proc. 34th AIAA Structures, Structural Dynamics, and Materials Conf., Part 4, pp. 1881-1889, J. struct. Optim. (Submitted).
-
Proc. 34th AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.4 PART
, pp. 1881-1889
-
-
Ley, R.P.1
Gürdal, Z.2
Johnson, E.R.3
-
27
-
-
0027266181
-
-
Submitted
-
R. P. Ley, Z. Gürdal and E. R. Johnson, Optimal design of imperfect anisotropic, ring-stiffened cylinders under combined loads. AIAA paper 93-1526-CP. Proc. 34th AIAA Structures, Structural Dynamics, and Materials Conf., Part 4, pp. 1881-1889, J. struct. Optim. (Submitted).
-
J. Struct. Optim.
-
-
-
28
-
-
0027224297
-
Postbuckling of laminated flat and curved panels under combined thermal and mechanical loadings
-
AIAA paper 93-1563-CP
-
L. Librescu, N. K. Chandiramani, M. P. Nemeth and J. H. Jr. Starnes, Postbuckling of laminated flat and curved panels under combined thermal and mechanical loadings. AIAA paper 93-1563-CP, Proc. 34th AIAA Structures, Structural Dynamics, and Materials Conf., pp. 2229-2239 (1993).
-
(1993)
Proc. 34th AIAA Structures, Structural Dynamics, and Materials Conf.
, pp. 2229-2239
-
-
Librescu, L.1
Chandiramani, N.K.2
Nemeth, M.P.3
Starnes J.H., Jr.4
-
29
-
-
0027316548
-
Classical versus non-classical postbuckling behavior of laminated composite panels under complex loading conditions
-
Edited by L. Librescu
-
L. Librescu, W. Lin, M. P. Nemeth and J. H. Jr. Starnes, Classical versus non-classical postbuckling behavior of laminated composite panels under complex loading conditions. In: Nonclassical Problems of the Theory and Behavior of Structures Exposed to Complete Environmental Conditions (Edited by L. Librescu), AMD Vol. 164, pp. 169-182 (1993).
-
(1993)
Nonclassical Problems of the Theory and Behavior of Structures Exposed to Complete Environmental Conditions
, vol.164 AMD
, pp. 169-182
-
-
Librescu, L.1
Lin, W.2
Nemeth, M.P.3
Starnes J.H., Jr.4
-
30
-
-
0027659587
-
Finite strip post-local-buckling analysis of composite prismatic plate structures
-
D. J. Dawe, S. S. E. Lam and Z. G. Azizian, Finite strip post-local-buckling analysis of composite prismatic plate structures. Comput. Struct. 48, 1011-1024 (1993).
-
(1993)
Comput. Struct.
, vol.48
, pp. 1011-1024
-
-
Dawe, D.J.1
Lam, S.S.E.2
Azizian, Z.G.3
-
31
-
-
0027665895
-
Post-buckling analysis of laminated stiffeners
-
H.-S. Shen and F. W. Williams, Post-buckling analysis of laminated stiffeners. Comput. Struct. 48, 1117-1124 (1993).
-
(1993)
Comput. Struct.
, vol.48
, pp. 1117-1124
-
-
Shen, H.-S.1
Williams, F.W.2
-
32
-
-
0027148192
-
Shell stability analysis in a computer aided engineering (CAE) environment
-
AIAA paper 93-1333-CP
-
J. Arbocz and J. M. A. M. Hol, Shell stability analysis in a computer aided engineering (CAE) environment. AIAA paper 93-1333-CP, Proc. 34th AIAA Structures, Structural Dynamics, and Materials Conf., Part 1, pp. 300-314 (1993).
-
(1993)
Proc. 34th AIAA Structures, Structural Dynamics, and Materials Conf.
, Issue.1 PART
, pp. 300-314
-
-
Arbocz, J.1
Hol, J.M.A.M.2
-
33
-
-
0029634382
-
Optimum design of composite stiffened panels under combined loading
-
D. Bushnell and W. D. Bushnell, Optimum design of composite stiffened panels under combined loading. Comput. Struct. 55, 819-856 (1995).
-
(1995)
Comput. Struct.
, vol.55
, pp. 819-856
-
-
Bushnell, D.1
Bushnell, W.D.2
-
34
-
-
0023167129
-
PANDA2-program for minimum weight design of stiffened, composite, locally buckled panels
-
D. Bushnell, PANDA2-program for minimum weight design of stiffened, composite, locally buckled panels. Comp. Struct. 25, 469-605 (1987). See also, Compt. Struct. 44, 1091-1119 (1992).
-
(1987)
Comp. Struct.
, vol.25
, pp. 469-605
-
-
Bushnell, D.1
-
35
-
-
0026909339
-
-
D. Bushnell, PANDA2-program for minimum weight design of stiffened, composite, locally buckled panels. Comp. Struct. 25, 469-605 (1987). See also, Compt. Struct. 44, 1091-1119 (1992).
-
(1992)
Compt. Struct.
, vol.44
, pp. 1091-1119
-
-
-
36
-
-
0023246690
-
Use of PANDA2 to optimize composite, imperfect, stiffened, locally buckled panels under combined in-plane loads and normal pressure
-
Edited by D. Hui and T. Kozik
-
D. Bushnell, Use of PANDA2 to optimize composite, imperfect, stiffened, locally buckled panels under combined in-plane loads and normal pressure. Design and Analysis of Composite Material Vessels, PVP Vol. 121 (Edited by D. Hui and T. Kozik), pp. 21-42 (1987).
-
(1987)
Design and Analysis of Composite Material Vessels
, vol.121 PVP
, pp. 21-42
-
-
Bushnell, D.1
-
37
-
-
0023531651
-
Theoretical basis of the PANDA computer program for preliminary design of stiffened panels under combined in-plane loads
-
D. Bushnell, Theoretical basis of the PANDA computer program for preliminary design of stiffened panels under combined in-plane loads. Comput. Struct. 27, 541-563 (1987).
-
(1987)
Comput. Struct.
, vol.27
, pp. 541-563
-
-
Bushnell, D.1
-
38
-
-
0043139935
-
-
Unpublished literature distributed with PANDA2
-
D. Bushnell, PANDA2.NEWS, Unpublished literature distributed with PANDA2.
-
PANDA2.NEWS
-
-
Bushnell, D.1
-
39
-
-
85029997427
-
-
D. Bushnell, Improvements to PANDA2, Vol. 1; Vol. 2, Part 1; Vol. 2, Part 2. Unpublished literature distributed with PANDA2.
-
Improvements to PANDA2
, vol.1
-
-
Bushnell, D.1
-
40
-
-
85029988105
-
-
D. Bushnell, Improvements to PANDA2, Vol. 1; Vol. 2, Part 1; Vol. 2, Part 2. Unpublished literature distributed with PANDA2.
-
Improvements to PANDA2
, vol.2
, Issue.1 PART
-
-
-
41
-
-
85029974651
-
-
Unpublished literature distributed with PANDA2
-
D. Bushnell, Improvements to PANDA2, Vol. 1; Vol. 2, Part 1; Vol. 2, Part 2. Unpublished literature distributed with PANDA2.
-
Improvements to PANDA2
, vol.2
, Issue.2 PART
-
-
-
42
-
-
0027558464
-
Optimization of composite, stiffened, imperfect panels under combined loads for service in the postbuckling regime
-
D. Bushnell, Optimization of composite, stiffened, imperfect panels under combined loads for service in the postbuckling regime. Comput. Meth. appl. Mech. Engng 103, 43-114 (1993).
-
(1993)
Comput. Meth. Appl. Mech. Engng
, vol.103
, pp. 43-114
-
-
Bushnell, D.1
-
44
-
-
0022715531
-
An element independent corotational procedure for the treatment of large rotations
-
C. C. Rankin and F. A. Brogan, An element independent corotational procedure for the treatment of large rotations. J. Pres. Ves. Tech. 108, 165-174.
-
J. Pres. Ves. Tech.
, vol.108
, pp. 165-174
-
-
Rankin, C.C.1
Brogan, F.A.2
-
45
-
-
0022736723
-
Post-buckling analysis using a general purpose code
-
G. A. Thurston, F. A. Brogan and P. Stehlin, Post-buckling analysis using a general purpose code. AIAA J. 24, 1013-1020 (1986).
-
(1986)
AIAA J.
, vol.24
, pp. 1013-1020
-
-
Thurston, G.A.1
Brogan, F.A.2
Stehlin, P.3
-
46
-
-
84872472328
-
-
NASA CR 4000, NASA Langley Research Center, Hampton, VA
-
C. C. Rankin, P. Stehlin, and F. A. Brogan, Enhancements to the STAGS computer code. NASA CR 4000, NASA Langley Research Center, Hampton, VA (1986).
-
(1986)
Enhancements to the STAGS Computer Code
-
-
Rankin, C.C.1
Stehlin, P.2
Brogan, F.A.3
-
47
-
-
0001814117
-
A general-purpose optimization program for engineering design
-
G. N. Vanderplaats and H. Sugimoto, A general-purpose optimization program for engineering design. Comput. Struct. 24, 13-21 (1986).
-
(1986)
Comput. Struct.
, vol.24
, pp. 13-21
-
-
Vanderplaats, G.N.1
Sugimoto, H.2
-
48
-
-
85007657813
-
Influence of edge conditions on the stability of axially compressed cylindrical shells
-
B. O. Almroth, Influence of edge conditions on the stability of axially compressed cylindrical shells. AIAA J. 4, 134-140 (1966).
-
(1966)
AIAA J.
, vol.4
, pp. 134-140
-
-
Almroth, B.O.1
-
49
-
-
0018943884
-
Effect of prebuckling deformations on buckling of laminated composite circular cylindrcial shells
-
R. M. Jones and J. C. F. Hennemann, Effect of prebuckling deformations on buckling of laminated composite circular cylindrcial shells. AIAA J. 18, 110-115 (1980). [See also, Proc. AIAA/ASME 19th SDM Conf. pp. 370-379 (1978).]
-
(1980)
AIAA J.
, vol.18
, pp. 110-115
-
-
Jones, R.M.1
Hennemann, J.C.F.2
-
50
-
-
0018943884
-
-
R. M. Jones and J. C. F. Hennemann, Effect of prebuckling deformations on buckling of laminated composite circular cylindrcial shells. AIAA J. 18, 110-115 (1980). [See also, Proc. AIAA/ASME 19th SDM Conf. pp. 370-379 (1978).]
-
(1978)
Proc. AIAA/ASME 19th SDM Conf.
, pp. 370-379
-
-
-
51
-
-
0001162463
-
The effect of axisymmetric imperfections on the buckling of cylindrical shells under axial compression
-
W. T. Koiter, The effect of axisymmetric imperfections on the buckling of cylindrical shells under axial compression. Kononkl. Ned. Akad. Wetenschap. Proc. B 66, 265-279 (1963).
-
(1963)
Kononkl. Ned. Akad. Wetenschap. Proc. B
, vol.66
, pp. 265-279
-
-
Koiter, W.T.1
-
52
-
-
0016034966
-
Stress, stability and vibration of complex, branched shells of revolution
-
D. Bushnell, Stress, stability and vibration of complex, branched shells of revolution. Comput. Struct. 4, 399-435 (1974).
-
(1974)
Comput. Struct.
, vol.4
, pp. 399-435
-
-
Bushnell, D.1
-
54
-
-
85029993346
-
-
Lockhead Missiles and Space Co., Inc., Palo Alto, California, a postprocessor for STAGS (not released as of this writing)
-
W. D. Bushnell, F. A. Brogan, H. Cabiness and C. Rankin, STAGSPP, Lockhead Missiles and Space Co., Inc., Palo Alto, California, a postprocessor for STAGS (not released as of this writing).
-
STAGSPP
-
-
Bushnell, W.D.1
Brogan, F.A.2
Cabiness, H.3
Rankin, C.4
-
55
-
-
0021606008
-
Some computational aspects of the stability analysis of nonlinear structures
-
E. Riks, Some computational aspects of the stability analysis of nonlinear structures. Comput. Meth. appl. Mech. 47, 219-259 (1984).
-
(1984)
Comput. Meth. Appl. Mech.
, vol.47
, pp. 219-259
-
-
Riks, E.1
-
56
-
-
0005892361
-
-
NASA CR 4360, NASA Langley Research Center, Hampton, VA
-
G. M. Stanley, K. C. Park and H. Cabiness, The computational structural mechanics testbed structural element processor ES7: revised ANS shell elements. NASA CR 4360, NASA Langley Research Center, Hampton, VA (1991).
-
(1991)
The Computational Structural Mechanics Testbed Structural Element Processor Es7: Revised Ans Shell Elements
-
-
Stanley, G.M.1
Park, K.C.2
Cabiness, H.3
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