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1

Vinson, Jack R. The Behavior of Shells Composed of Isotropic and Composite Materials. Dordrecht: Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-015-8141-7.

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2

Vinson, Jack R. The behavior of shells composed of isotropic and composite materials. Dordrecht: Kluwer Academic Publishers, 1993.

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3

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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4

Illg, Walter. Effect of partial interlaminar bonding on impact resistance and loaded-hole behavior of graphite/epoxy quasi-isotropic laminates. Hampton, Va: Langley Research Center, 1986.

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5

Illg, Walter. Effects of partial interlaminar bonding on impact resistance and loaded hole behavior of graphite/epoxy quasi-isotropic laminates. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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6

Behavior of Sandwich Structures of Isotropic and Composite Materials. CRC Press LLC, 2018.

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7

Behavior of Sandwich Structures of Isotropic and Composite Materials. CRC Press LLC, 2018.

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8

Vinson, JackR. Behavior of Sandwich Structures of Isotropic and Composite Materials. CRC Press LLC, 2018.

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9

Vinson, JackR. Behavior of Sandwich Structures of Isotropic and Composite Materials. CRC Press LLC, 2018.

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10

Vinson, Jack R. Behavior of Shells Composed of Isotropic and Composite Materials. Springer, 2013.

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11

Behavior of Sandwich Structures of Isotropic and Composite Materials. Routledge, 1999.

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12

The behavior of sandwich structures of isotropic and composite materials. Lancaster, Pa: Technomic Pub. Co., 1999.

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13

Vinson, Jack R. The Behavior of Shells Composed of Isotropic and Composite Materials. Springer Netherlands, 2009.

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14

National Aeronautics and Space Administration (NASA) Staff. Buckling and Postbuckling Behavior of Compression-Loaded Isotropic Plates with Cutouts. Independently Published, 2018.

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15

Fatigue Behavior of a Quasi-Isotropic Graphite/Epoxy Laminate Embedded with a Piezoelectric Sensor. Storming Media, 1997.

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16

Delamination behavior of quasi-isotropic graphite epoxy laminates subjected to tension and torsion loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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17

Electro-Mechanical Fatigue Behavior of a Quasi-Isotropic Laminate with an Embedded Piezoelectric Actuator. Storming Media, 1998.

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18

Sjerve, Eric. Polarization behaviour of the quasi-isotropic 3.39 [mi]m (J-1 to J-2) helium-neon Zeeman laser. 1996.

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