Effects of static tensile load on the thermal expansion of Gr/PI composite material by Gary L Farley

Cover of: Effects of static tensile load on the thermal expansion of Gr/PI composite material | Gary L Farley

Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .

Written in English

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Subjects:

  • Composite materials -- Testing,
  • Laminated materials -- Testing,
  • Strains and stresses

Edition Notes

Book details

StatementGary L. Farley
SeriesNASA technical paper -- 1867, AVRADCOM technical report -- 81-B-2, AVRADCOM technical report -- 81-B-2
ContributionsUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Army Research and Technology Laboratories (U.S.). Structures Laboratory
The Physical Object
Pagination32 p. :
Number of Pages32
ID Numbers
Open LibraryOL14932945M

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The effect of static tensile load on the thermal expansion of Gr/PI comĀ­ posite material was measured for seven different laminate configurations. A computer program was developed which implements laminate theory in a piecewise linear fashion to predict the coupled nonlinear thermomechanical behavior.

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Effects of static tensile load on the thermal expansion of Gr/PI composite material / (Washington, D.C.: National Aeronautics and Space Administration, Scientific and.

Filed under: Composite materials. Engineering and the Advancement of Human Welfare: 10 Outstanding Achievements,by National Academy of Engineering (page images at NAP) Composite materials: a compilation / ([Washington]: NASA ; Springfield, Va.: for sale by the National Technical Information Service ;, ), by United States.

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Full text of "NASA Technical Reports Server (NTRS) Structural Framework for Flight: NASA's Role in Development of Advanced Composite Materials for. Full text of "DTIC ADA Proceedings of the Ninth United States - Japan Conference on Composite Materials" See other formats.

Compressive strain is a result of the high temperatures of the CVD process in company with the negative thermal expansion coefficient of graphene. 3]), deposition [5] and composite production. Full text of "NASA scientific and technical publications: A catalog of Special Publications, Reference Publications, Conference Publications, and Technical Papers, " See other formats.

Prepublioation issue for EPA libraries and State Solid Waste Management Agencies EUROPEAN REFUSE-FIRED ENERGY SYSTEMS Evaluation of Design Practices Volume 2 This report (SWC.2) describes work performed for the Office of Solid Waste under contract no. and is reproduced as received from the contractor.

Failure of composite plates under static biaxial planar loading. NASA Technical Reports Server (NTRS) Waas, Anthony M.; Khamseh, Amir R. The project involved detailed. Effects of static tensile load on the thermal expansion of Gr/PI composite material. NASA Technical Reports Server (NTRS) Farley, G.

The effect of static tensile load on the thermal expansion of Gr/PI composite material was measured for seven different laminate configurations. A computer program was developed which implements. designs which exploited the low coefficient of thermal expansion characteristics of the graphite composites.

The fuselage is a more conventional skin-stringer and frame design. The material usage for the primarily composite material design is shown in table V.

The advanced composite usage represents 55 percent of the total structural weight.

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