Repair Procedures for Advanced Composite Structures.

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Abstract:

The objective of this program is to develop repair technology that can be used to restore the structural integrity of damaged graphite-epoxy and hybrid composite aircraft structure. Research is being conducted to identify and classify damage, to perform repairs compatible with strength and functional requirements, and to verify the strength and durability of repaired structure.

Author(s):
No Author(s) Identified
Author Organization(s):
GENERAL DYNAMICS FORT WORTH TX FORT WORTH DIV
Descriptive Note:
Quarterly progress rept. no. 3, 11 Dec 74-10 Mar 75,
Pagination:
0084

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved Ofr Public Release; Distribution Unlimited.

RECORD

Collection: TR
Identifying Numbers
Contract/Grant Number(s):
F33615-74-C-5133
 Subject Terms
Joint Capability Areas:
JCA_5.3_Planning; JCA_5_Command and Control
Communities of Interest:
Air Platforms
Descriptor(s):
COMPOSITE AIRCRAFT, COMPOSITE STRUCTURES, FUNCTIONS, HYBRID SYSTEMS, RELIABILITY, REPAIR, REQUIREMENTS, STRUCTURAL PROPERTIES
Field(s)/Group(s):
Aircraft, Laminates and Composite Materials
Keyword(s):
U A reports
Report Date:
1975 Mar 20