Investigating the effects aviation fluids have on the flatwise compressive strength of Nomex® honeycomb core material

Composite honeycomb sandwich structure is widely used for aircraft structures such as control surfaces, radomes, engine cowls, and aircraft interior structure because of its lightweight and high strength characteristics. One of the disadvantages of honeycomb sandwich structure is that they are prone to fluid intrusion. The purpose of this study is to determine if the structural properties of honeycomb core are affected by contact with a fluid. The test specimens were manufactured of fiberglass prepreg for the facesheets and Nomex (R) honeycomb core for the core material in accordance with ASTM C-365/365M. Test specimens were soaked in several different kinds of fluids, such as aircraft fuel, turbine engine oil, hydraulic fluid, and water for a period of 60 days. Some of specimens were tested right after soaking period ended, and some of them were dried before they were tested. A flatwise compressive test was performed, and the test results were analyzed to determine how the contact with aircraft fluids affected the compressive strength of the Nomex (R) honeycomb core and how the strength was recovered when the specimens were dry. In addition, the investigation of de-bonding between facesheet and core material after soaking was performed to support the study.

Automated summary

The study investigates the influence of fluid contact on the structural properties of honeycomb core in composite honeycomb sandwich structures. Test specimens were soaked in different fluids, tested for compressive strength after soaking and drying, and analyzed for the effects of aircraft fluids on Nomex (R) honeycomb core compressive strength and recovery after drying. Debonding between facesheet and core material after soaking was also examined to support the study.