Determination of the Principal Mechanical Properties of Reinforced Plastic Laminates for Aircraft.

reportActive / Technical Report | Accession Number: ADA043350 | Open PDF

Abstract:

The purpose of the test program described in this report was to develop engineering data on the mechanical and physical properties of reinforced plastic laminates for aircraft. Following are the systems tested Modmor I GraphiteNarmco 5208 AS GraphiteHercules 3501-5 T300 GraphiteNarmco 5208 RAC-73501014S-24 Kevlar 49 PRD IIIHexcel F161. The laminates were subjected to the following tests tension, fatigue, compression, in-plane shear, flexural and interlaminar shear, and bearing stress. Author

Author(s):
Hofer, K. E.
Author Organization(s):
IIT RESEARCH INST CHICAGO ILL
Descriptive Note:
Final technical rept. Oct 73-Apr 77,
Pagination:
0046

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Contract/Grant Number(s):
DAAA21-74-C-0114
 Subject Terms
Joint Capability Areas:
JCA_4.5.4_Requirements Definition; JCA_4.5_Operational Contract Support; JCA_5_Command and Control; JCA_1_Force Support; JCA_4.6_Engineering; JCA_6_Net Centric
Modernization Areas:
Microelectronics
Communities of Interest:
Air Platforms
Descriptor(s):
*AIRCRAFT PANELS, *LAMINATED PLASTICS, *REINFORCED PLASTICS, MECHANICAL PROPERTIES, TENSILE STRENGTH, PHYSICAL PROPERTIES, COMPOSITE MATERIALS, STRESS TESTING, TEST METHODS, BEARING STRENGTH, FATIGUE TESTS(MECHANICS), COMPRESSIVE PROPERTIES, SHEAR TESTS
Field(s)/Group(s):
Aircraft, Laminates and Composite Materials
Keyword(s):
LPN IITRI D6092
Report Date:
1977 Apr 01