Add to ORKGRepair techniques for graphite/epoxy and graphite/polyimide composite structures are discussed. Tension and compression test results for several basic repair processes that were applied to damaged specimens are shown to approach the strength of undamaged specimens. Other repair configurations currently under investigation are illustrated, and plans in the repair technology program are presented
The residual strength of specimens with damage and the sensitivity to damage while subjected to an a...
In aerospace engineering applications, lightweight material structures are considered to perform dif...
Development of repair technology is vital to the long-term application of new structural concepts on...
The large stiffness-to-weight and strength-to-weight ratios of graphite composite in combination wit...
A series of tests was conducted to measure the strength of stitched carbon/epoxy composites containi...
The X-29 experimental aircraft, based at the NASA Dryden Flight Research Facility, Edwards Air Force...
Commercial aircraft advanced composite wing surface panels were tested for durability and damage tol...
The purpose of composite repair development at KSC (John F. Kennedy Space Center) is to provide supp...
Results are presented from an experimental evaluation of IM7/8551-7 and IM6/18081, two new toughened...
Tests were performed assessing the effectiveness of repair in restoring the mechanical properties of...
This presentation discusses the development and results of composite patch repair perfromed at Kenne...
Under the NASA-sponsored contracts for Advanced Technology Composite Aircraft Structures (ATCAS) and...
Fiber reinforced composites are being extensively used for aircraft structural application by virtue...
The influence of three different resin systems on the damage tolerance of graphite/polymer laminates...
This report addresses the various issues that are to be considered in arriving at an effective repai...
The residual strength of specimens with damage and the sensitivity to damage while subjected to an a...
In aerospace engineering applications, lightweight material structures are considered to perform dif...
Development of repair technology is vital to the long-term application of new structural concepts on...
The large stiffness-to-weight and strength-to-weight ratios of graphite composite in combination wit...
A series of tests was conducted to measure the strength of stitched carbon/epoxy composites containi...
The X-29 experimental aircraft, based at the NASA Dryden Flight Research Facility, Edwards Air Force...
Commercial aircraft advanced composite wing surface panels were tested for durability and damage tol...
The purpose of composite repair development at KSC (John F. Kennedy Space Center) is to provide supp...
Results are presented from an experimental evaluation of IM7/8551-7 and IM6/18081, two new toughened...
Tests were performed assessing the effectiveness of repair in restoring the mechanical properties of...
This presentation discusses the development and results of composite patch repair perfromed at Kenne...
Under the NASA-sponsored contracts for Advanced Technology Composite Aircraft Structures (ATCAS) and...
Fiber reinforced composites are being extensively used for aircraft structural application by virtue...
The influence of three different resin systems on the damage tolerance of graphite/polymer laminates...
This report addresses the various issues that are to be considered in arriving at an effective repai...
The residual strength of specimens with damage and the sensitivity to damage while subjected to an a...
In aerospace engineering applications, lightweight material structures are considered to perform dif...
Development of repair technology is vital to the long-term application of new structural concepts on...