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The structural behavior of a graphite-polymide honeycomb sandwich panel with quasi-isotropic face sheets and an orthotropic coreThe results of a series of tests of graphite-polyimide honeycomb sandwich panels are presented. The panels were 1.22 m long, 0.508 m wide, and approximately 13.3 m thick. The face sheets were a T-300/PMR-15 fabric in a quasi-isotropic layup and were 0.279 mm thick. The core was Hexcel HRH 327-3/16 - 4.0 glass reinforced polyimide honeycomb, 12.7 mm thick. Three panels were used in the test: one was cut into smaller pieces for testing as beam, compression, and shear specimens; a second panel was used for plate bending tests; the third panel was used for in-plane stability tests. Presented are the experimental results of four point bending tests, short block compression tests, core transverse shear modulus, three point bending tests, vibration tests, plate bending tests, and panel stability tests. The results of the first three tests are used to predict the results of some of the other tests. The predictions and experimental results are compared, and the agreement is quite good.
Document ID
19800017899
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hyer, M. W.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Hagaman, J. A.
(Old Dominion Univ. Research Foundation)
Date Acquired
September 4, 2013
Publication Date
June 1, 1979
Subject Category
Composite Materials
Report/Patent Number
VPI-E-79-23
NASA-CR-163297
Report Number: VPI-E-79-23
Report Number: NASA-CR-163297
Accession Number
80N26398
Funding Number(s)
CONTRACT_GRANT: NSG-1167
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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