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1

Shama, Mohamed. Buckling of Ship Structures. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013.

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2

Delamination buckling of composite materials. Dordrecht: Kluwer, 1988.

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3

Johann, Arbocz, and Weller T, eds. Buckling experiments: Experimental methods in buckling of thin-walled structures. Chichester: Wiley, 1998.

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4

Akbarov, Surkay. Stability Loss and Buckling Delamination: Three-Dimensional Linearized Approach for Elastic and Viscoelastic Composites. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013.

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5

Stein, Manuel. Postbuckling response of long thick plates loaded in compression including higher order transverse shearing effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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6

Hyer, M. W. Innovative design of composite structures: The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University, 1990.

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7

Hyer, M. W. Innovative design of composite structures: The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University, 1990.

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8

Hyer, M. W. Innovative design of composite structures: Further studies in the use of a curvilinear fiber format to improve structural efficiency. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1988.

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9

Hyer, M. W. Innovative design of composite structures: Design, manufacturing, and testing of plates utilitzing [sic] curvilinear fiber trajectories : final report for NASA. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University ; Hampton, VA, 1994.

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10

Hyer, M. W. Innovative design of composite structures: Axisymmetric deformations of unsymmetrically laminated cylinders loaded in axial compression : semiannual status report. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1990.

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11

Hyer, M. W. Innovative design of composite structures: The use of curvilinear fiber format in composite structure design. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University, 1990.

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12

Shama, Mohamed. Buckling of Ship Structures. Springer, 2014.

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13

Shama, Mohamed. Buckling of Ship Structures. Springer, 2012.

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14

Kachanov, L. M. Delamination Buckling of Composite Materials. Springer, 2012.

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15

Bian Huazhong University of Science and. Topological Optimization of Buckling. De Gruyter, 2018.

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16

R, Johnson Eric, Starnes James H, and United States. National Aeronautics and Space Administration., eds. Local buckling and crippling of composite stiffener sections. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1988.

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17

Arbocz, J., T. Weller, and J. Singer. Buckling Experiments, Shells, Built-up Structures, Composites and Additional Topics (Buckling Experiments). Wiley, 2002.

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18

E, Grady Joseph, and United States. National Aeronautics and Space Administration., eds. A NASTRAN DMAP alter for linear buckling analysis under dynamic loading. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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19

User manual for VICONOPT: An exact analysis and optimum design program covering the buckling and vibration of prismatic assemblies of flat in-plane loaded, anisotropic plates with approximations for discrete supports and transverse stiffeners. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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20

W, Hyer M., and United States. National Aeronautics and Space Administration., eds. Postbuckling failure of composite plates with central holes. Blacksburg, Va: Virginia Polytechnic Institute and State University, 1992.

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21

Structural analysis and design of geodesically stiffened composte panels with variable stiffener distribution. [Washington, DC: National Aeronautics and Space Administration, 1992.

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22

Zafer, Gürdal, and United States. National Aeronautics and Space Administration., eds. Optimal design of geodesically stiffened composite cylindrical shells. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1992.

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23

Fracture toughness computational simulation of general delaminations in fiber composites. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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24

W, Hyer M., Starnes James H, and United States. National Aeronautics and Space Administration., eds. Numerical and experimental investigation of the bending response of thin-walled composite cylinders. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1993.

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25

N, Shivakumar K., and Langley Research Center, eds. Strain-energy release rate analysis of a laminate with a postbuckled delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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26

Strain-energy release rate analysis of a laminate with a postbuckled delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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27

Kubiak, Tomasz. Static and Dynamic Buckling of Thin-Walled Plate Structures. Springer, 2013.

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28

Kubiak, Tomasz. Static and Dynamic Buckling of Thin-Walled Plate Structures. Springer, 2016.

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29

Kubiak, Tomasz. Static and Dynamic Buckling of Thin-Walled Plate Structures. 2013.

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30

Center, Langley Research, ed. Short-wavelength buckling and shear failures for compression-loaded composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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31

Short-wavelength buckling and shear failures for compression-loaded composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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32

Short-wavelength buckling and shear failures for compression-loaded composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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33

Buckling behavior of long symmetrically laminated plates subjected to combined loadings. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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34

Failure criteria and analysis in dynamic response: Presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Dallas, Texas, November 25-30, 1990. New York, N.Y: ASME, 1990.

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35

Ga.) American Society of Mechanical Engineers. Winter Meeting (1991 : Atlanta. Failure Criteria and Analysis in Dynamic Response: Presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Dallas, Texas, November 25-30, 1990 (Cat No G00528). Amer Society of Mechanical, 1990.

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36

Center, Langley Research, ed. Buckling and postbuckling behavior of compression-loaded isotropic plates with cutouts. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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37

Center, Langley Research, ed. Buckling and postbuckling behavior of square compression-loaded graphite-epoxy plates with circular cutouts. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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38

Daniel, Sydow P., Librescu Liviu, and Langley Research Center, eds. Postbuckling response of long thick plates loaded in compression including higher order transverse shearing effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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39

1938-, Noor Ahmed Khairy, American Society of Mechanical Engineers. Aerospace Division., American Society of Mechanical Engineers. Pressure Vessels and Piping Division., and International Mechanical Engineering Congress and Exposition (1994 : Chicago, Ill.), eds. Buckling and postbuckling of composite structures: Presented at 1994 International Mechanical Engineering Congress and Exposition, Chicago, Illinois, November 6-11, 1994. New York, N.Y: American Society of Mechanical Engineers, 1994.

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40

American Society of Mechanical Engineers. Pressure Vessels and Piping Division and Ga.) International Mechanical Engineering Congress and Exposition (1996 : Atlanta. Buckling & Postbuckling of Composite Structures: 1994 International Mechanical Engineering Congress & Expostion, Chicago, Illinois - November 6-11, 1994 (Ad - Pvp Ser. ; Vol. 41, Vol. 293). American Society of Mechanical Engineers, 1994.

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41

Legendre, Laurent, and Douglas W. Darnowski. Biotechnology with carnivorous plants. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198779841.003.0020.

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Abstract:
Several carnivorous plant families have been a source of medicine for centuries in many parts of the world. Research into their active ingredients have revealed that they include naphthoquinones, flavonoids, phenolic acid derivatives, goodyerosides, iridoids, and phenylpropanoids. Many aspects of their industrial production have been optimized, including plant elicitation, plant genetic modification, and plant in vitro culture to limit the collect of wild material. The currently most active biotechnological developments are related directly to their carnivorous nature. These include the heterologous production of therapeutic polypeptides by carnivorous plant secretory glands; and the creation of bio-inspired engineered products based on the snap-buckling mechanism of trap closure of the Venus’ fly trap, the internal nano-structures of the Drosera mucilage, and the physical properties of the slippery zone of the Nepenthes pitcher with applications in the textile, automobile, aeronautics, architecture, and medical industries.
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42

F, Card Michael, and United States. National Aeronautics and Space Administration., eds. Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells: Presented at the AIAA/ASCE/ASC 36th Structures, Structural Dynamics and Materials Conference, April 10-12, 1995, New Orleans, LA, Thermal Structures Category. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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43

F, Card Michael, and United States. National Aeronautics and Space Administration., eds. Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells: Presented at the AIAA/ASCE/ASC 36th Structures, Structural Dynamics and Materials Conference, April 10-12, 1995, New Orleans, LA, Thermal Structures Category. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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