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Laminates

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Online Results (47)
1.
An analytical method to calculate effective elastic properties of general multifunctional honeycomb cores in sandwich composites
Author
Saether, Erik
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2019.
Online
https://purl.fdlp.gov/GPO/gpo121341
Location
Yale Internet Resource >> None
Format
Books / Online
2.
Computational performance of progressive damage analysis of composite laminates using Abaqus/Explicit with 16 to 512 CPU cores
Author
Bergan, A. C.
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 2019.
Online
https://purl.fdlp.gov/GPO/gpo118412
Location
Yale Internet Resource >> None
Format
Books / Online
3.
Static torsion testing and modeling of a variable thickness hybrid composite bull gear
Author
Johnston, Joel P.
Published
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2019.
Online
https://purl.fdlp.gov/GPO/gpo130306
Location
Yale Internet Resource >> None
Format
Books / Online
4.
AF-Shell 1.0 user guide
Author
McElroy, Mark W.
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2017.
Online
https://purl.access.gpo.gov/GPO/gpo85735
Location
Yale Internet Resource >> None
Format
Books / Online
5.
Influence of shear stiffness degradation on crack paths in uni-directional composite laminates
Author
Satyanarayana, Arunkumar
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2017.
Online
https://purl.fdlp.gov/GPO/gpo87610
Location
Yale Internet Resource >> None
Format
Books / Online
6.
An enriched shell finite element for progressive damage simulation in composite laminates
Author
McElroy, Mark W.
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2016.
Online
http://purl.fdlp.gov/GPO/gpo77403
Location
Yale Internet Resource >> None
Format
Books / Online
7.
Multiscale static analysis of notched and unnotched laminates using the generalized method of cells
Author
Ghezeljeh, Paria Naghipour
Published
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2016.
Online
http://purl.fdlp.gov/GPO/gpo71786
Location
Yale Internet Resource >> None
Format
Books / Online
8.
An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders
Author
Nemeth, Michael P.
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013.
Online
http://purl.fdlp.gov/GPO/gpo45682
Location
Yale Internet Resource >> None
Format
Books / Online
9.
Combining through-thickness reinforcement and self-healing for improved damage tolerance and durability of composites
Author
O'Brien, T. Kevin
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013.
Online
http://purl.fdlp.gov/GPO/gpo38001
Location
Yale Internet Resource >> None
Format
Books / Online
10.
Normalization of impact energy by laminate thickness for compression after impact testing
Author
Nettles, A. T. (Alan T.)
Published
Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, 2013.
Online
http://purl.fdlp.gov/GPO/gpo37983
Location
Yale Internet Resource >> None
Format
Books / Online
11.
Ultrasonic nondestructive evaluation of PRSEUS pressure cube article in support of load test to failure
Author
Johnston, Patrick H.
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013.
Online
http://purl.fdlp.gov/GPO/gpo37998
Location
Yale Internet Resource >> None
Format
Books / Online
12.
Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
Online
http://purl.fdlp.gov/GPO/gpo28010
Location
Yale Internet Resource >> None
Format
Books / Online
13.
Computational implementation of a thermodynamically based work potential model for progressive microdamage and transverse cracking in fiber-reinforced laminates
Published
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Online
http://purl.fdlp.gov/GPO/gpo30591
Location
Yale Internet Resource >> None
Format
Books / Online
14.
Conditions for symmetries in the buckle patterns of laminated-composite plates
Author
Nemeth, Michael P.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
Online
http://purl.fdlp.gov/GPO/gpo30943
Location
Yale Internet Resource >> None
Format
Books / Online
15.
Cubic zig-zag enrichment of the classical Kirchhoff kinematics for laminated and sandwich plates
Author
Nemeth, Michael P.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
Online
http://purl.fdlp.gov/GPO/gpo28057
Location
Yale Internet Resource >> None
Format
Books / Online
16.
The exact solution for linear thermoelastic axisymmetric deformations of generally laminated circular cylindrical shells
Author
Nemeth, Michael P.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
Online
http://purl.fdlp.gov/GPO/gpo33345
Location
Yale Internet Resource >> None
Format
Books / Online
17.
Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage
Author
Hodge, A. J.
Published
[Huntsville], Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
Online
http://purl.fdlp.gov/GPO/gpo11790
Location
Yale Internet Resource >> None
Format
Books / Online
18.
Numerical implementation of a multiple-ISV thermodynamically-based work potential theory for modeling progressive damage and failure in fiber-reinforced laminates
Author
Pineda, Evan J.
Published
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
Online
http://purl.fdlp.gov/GPO/gpo24418
Location
Yale Internet Resource >> None
Format
Books / Online
19.
Probabilistic simulation for combined thermo-mechanical cyclic fatigue in composites
Author
Chamis, C. C. (Christos C.)
Published
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
Online
http://purl.fdlp.gov/GPO/gpo20421
Location
Yale Internet Resource >> None
Format
Books / Online
20.
A treatise on equivalent-plate stiffnesses for stiffened laminated-composite plates and plate-like lattices
Author
Nemeth, Michael P.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
Online
http://purl.fdlp.gov/GPO/gpo9439
Location
Yale Internet Resource >> None
Format
Books / Online
21.
Nondimensional parameters and equations for nonlinear and bifurcation analyses of thin anisotropic quasi-shallow shells
Author
Nemeth, Michael P.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2010]
Online
http://purl.fdlp.gov/GPO/gpo4820
Location
Yale Internet Resource >> None
Format
Books / Online
22.
Probabilistic methods for structural reliability and risk
Author
Chamis, C. C. (Christos C.)
Published
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Online
http://purl.fdlp.gov/GPO/gpo624
Location
Yale Internet Resource >> None
Format
Books / Online
23.
Modeling of unit-cells with Z-Pins using FLASH pre-processing and post-processing
Author
Krueger, Ronald
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2005]
Online
http://purl.fdlp.gov/GPO/gpo180
Location
Yale Internet Resource >> None
Format
Books / Online
24.
A multilayered thin film insulator for harsh environments
Author
Wrbanek, John D.
Published
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2002.
Online
http://purl.access.gpo.gov/GPO/LPS36334
Location
Yale Internet Resource >> None
Format
Books / Online
25.
A multilayered thin film insulator for harsh environments
Published
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2002]
Online
Adobe Acrobat Reader required
Location
SML, Microform (Non-Circulating) >> NAS 1.15:211873
Format
Books / Microforms