-
1
-
-
0242525583
-
Biologically inspired technologies
-
San Diego, CA, March
-
McGowan AR, Cox DE, Lazos BS, Waszak MR, Raney DL, Siochi EJ, et al. Biologically inspired technologies. In: NASA's morphing project, proceedings of SPIE smart structures and materials conference. San Diego, CA, March, 2003. p. 1-13.
-
(2003)
NASA's morphing project, proceedings of SPIE smart structures and materials conference
, pp. 1-13
-
-
McGowan, A.R.1
Cox, D.E.2
Lazos, B.S.3
Waszak, M.R.4
Raney, D.L.5
Siochi, E.J.6
-
3
-
-
0036029825
-
Identification of military morphing aircraft missions and morphing technology assessment
-
San Diego, CA, March
-
Bowman J, Sanders B, Weisshaar T. Identification of military morphing aircraft missions and morphing technology assessment. In: Proceedings of SPIE smart materials and structures conference. San Diego, CA, March, 2002. p. 121-32.
-
(2002)
Proceedings of SPIE smart materials and structures conference
, pp. 121-132
-
-
Bowman, J.1
Sanders, B.2
Weisshaar, T.3
-
4
-
-
0036850488
-
Review of state of art of smart structures and integrated systems
-
Chopra I. Review of state of art of smart structures and integrated systems. AIAA J 40 11 (2002) 2145-2187
-
(2002)
AIAA J
, vol.40
, Issue.11
, pp. 2145-2187
-
-
Chopra, I.1
-
5
-
-
0039715728
-
Deformation mechanisms in negative Poisson's ratio materials: structural aspects
-
Lakes R.S. Deformation mechanisms in negative Poisson's ratio materials: structural aspects. J Mater Sci 26 (1991) 2287-2292
-
(1991)
J Mater Sci
, vol.26
, pp. 2287-2292
-
-
Lakes, R.S.1
-
6
-
-
0031103039
-
Properties of a chiral honeycomb with a Poisson's ratio of -1
-
Prall D., and Lakes R.S. Properties of a chiral honeycomb with a Poisson's ratio of -1. Int J Mech Sci 39 3 (1997) 305-314
-
(1997)
Int J Mech Sci
, vol.39
, Issue.3
, pp. 305-314
-
-
Prall, D.1
Lakes, R.S.2
-
8
-
-
34548606153
-
Numerical and experimental analysis of the static compliance of chiral truss-core airfoils
-
Spadoni A., and Ruzzene M. Numerical and experimental analysis of the static compliance of chiral truss-core airfoils. J Mech Mater Struct 2 5 (2007) 965
-
(2007)
J Mech Mater Struct
, vol.2
, Issue.5
, pp. 965
-
-
Spadoni, A.1
Ruzzene, M.2
-
9
-
-
75149126223
-
Static aeroelastic response of chiral truss-core airfoils
-
Spadoni A., and Ruzzene M. Static aeroelastic response of chiral truss-core airfoils. J Intell Mater Syst Struct (2007) 5
-
(2007)
J Intell Mater Syst Struct
, pp. 5
-
-
Spadoni, A.1
Ruzzene, M.2
-
10
-
-
44349149148
-
The hexachiral prismatic wingbox concept
-
Martin J., Heyder-Bruckner J.J., Remillat C., Scarpa F., Potter K., and Ruzzene M. The hexachiral prismatic wingbox concept. Phys Status Solidi B 245 3 (2008) 570-577
-
(2008)
Phys Status Solidi B
, vol.245
, Issue.3
, pp. 570-577
-
-
Martin, J.1
Heyder-Bruckner, J.J.2
Remillat, C.3
Scarpa, F.4
Potter, K.5
Ruzzene, M.6
-
11
-
-
33750175105
-
Dynamic response of chiral trus-core assemblies
-
Spadoni A., Ruzzene M., and Scarpa F. Dynamic response of chiral trus-core assemblies. J Intell Mater, Syst Struct 17 11 (2006) 941-952
-
(2006)
J Intell Mater, Syst Struct
, vol.17
, Issue.11
, pp. 941-952
-
-
Spadoni, A.1
Ruzzene, M.2
Scarpa, F.3
-
12
-
-
75149142537
-
-
ANSYSr. Theory Reference. ANSYS Academic Research, Release 11.0, 2007
-
ANSYSr. Theory Reference. ANSYS Academic Research, Release 11.0, 2007.
-
-
-
-
13
-
-
75149134432
-
-
Composite material handbook, 2. Polymer matrix composite materials properties. MIL-HDBK-17-2E, 1999, Department of Defense, USA.
-
Composite material handbook, vol. 2. Polymer matrix composite materials properties. MIL-HDBK-17-2E, 1999, Department of Defense, USA.
-
-
-
-
14
-
-
0030417381
-
Advances in elastomeric tooling technology
-
Sala G. Advances in elastomeric tooling technology. Mater Des 17 1 (1996) 33-42
-
(1996)
Mater Des
, vol.17
, Issue.1
, pp. 33-42
-
-
Sala, G.1
-
15
-
-
0025244734
-
Thermal properties of carbon-filled silicone rubbers for use in thermal expansion moulding
-
Richards J.M., Wostenholm G.H., Yates B., Darby M.I., and Phillips L.N. Thermal properties of carbon-filled silicone rubbers for use in thermal expansion moulding. J Mater Sci 25 (1990) 721-724
-
(1990)
J Mater Sci
, vol.25
, pp. 721-724
-
-
Richards, J.M.1
Wostenholm, G.H.2
Yates, B.3
Darby, M.I.4
Phillips, L.N.5
-
16
-
-
63749102878
-
Analysis and User's Manual
-
Version 6.7. Dassault System
-
Abaqus. Analysis and User's Manual Version 6.7. Dassault System, 2007.
-
(2007)
-
-
Abaqus1
-
17
-
-
16244423085
-
Progressive analyses of skin/stringer debonding
-
Blacksburg, VA, September
-
Davila CG, Camanho PP, de Moura MSFS. Progressive analyses of skin/stringer debonding. In: Proceedings of American society for composites, 16th technical conference. Blacksburg, VA, September, 2001.
-
(2001)
Proceedings of American society for composites, 16th technical conference
-
-
Davila, C.G.1
Camanho, P.P.2
de Moura, M.S.F.S.3
-
18
-
-
44749087315
-
Crack equivalent concept applied to the fracture characterization of bonded joints under pure mode I loading
-
De Moura M.F.S.F., Campilho R.D.S.G., and Gonçalves J.P.M. Crack equivalent concept applied to the fracture characterization of bonded joints under pure mode I loading. Compos Sci Technol 68 (2008) 2224-2230
-
(2008)
Compos Sci Technol
, vol.68
, pp. 2224-2230
-
-
De Moura, M.F.S.F.1
Campilho, R.D.S.G.2
Gonçalves, J.P.M.3
-
19
-
-
33847744149
-
An engineering solution for mesh size effect in the simulation of delamination using cohesive zone models
-
Turon A., Davila C.G., Camanho P.P., and Costa J. An engineering solution for mesh size effect in the simulation of delamination using cohesive zone models. Eng Fract Mech 74 (2007) 1665-1682
-
(2007)
Eng Fract Mech
, vol.74
, pp. 1665-1682
-
-
Turon, A.1
Davila, C.G.2
Camanho, P.P.3
Costa, J.4
-
20
-
-
84878507776
-
Experimental and numerical investigation on the failure modes of thick composite laminates
-
Hamburg, Germany, September
-
Airoldi A, Sala G, Pasqualini F. Experimental and numerical investigation on the failure modes of thick composite laminates. In: Proceedings of 25th congress of aeronautical science, ICAS 2006, Hamburg, Germany, 2006, September.
-
(2006)
Proceedings of 25th congress of aeronautical science, ICAS
-
-
Airoldi, A.1
Sala, G.2
Pasqualini, F.3
-
21
-
-
45449092359
-
Numerical simulation of sandwich T-joints under dynamic loading
-
Zhou D.W., Louca L.A., and Saunders M. Numerical simulation of sandwich T-joints under dynamic loading. Composites Part B 39 (2008) 973-985
-
(2008)
Composites Part B
, vol.39
, pp. 973-985
-
-
Zhou, D.W.1
Louca, L.A.2
Saunders, M.3
-
23
-
-
75149112832
-
-
American Society for Testing Materials. Standard test method for mixed mode I-mode II interlaminar fracture of unidirectional fiber reinforced polymer matrix composites. ASTM D 6671-01, 2001.
-
American Society for Testing Materials. Standard test method for mixed mode I-mode II interlaminar fracture of unidirectional fiber reinforced polymer matrix composites. ASTM D 6671-01, 2001.
-
-
-
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