Publication Date:
2019-06-27
Description:
Fire resistance mechanical property tests were conducted on sandwich configurations composed of resin-fiberglass laminates bonded with adhesives to Nomex honeycomb core. The test results were compared to proposed and current requirements for aircraft floor panel applications to demonstrate that the fire safety of the airplane could be improved without sacrificing mechanical performance of the aircraft floor panels.
Keywords:
COMPOSITE MATERIALS
Type:
NASA-CR-147750
Format:
application/pdf
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