Searched for: subject%3A%22shear%22
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document
Hagenbeek, M. (author), Sinke, J. (author)
Heated GLARE, a Fibre Metal Laminate with an integrated heater element, has a promising potential as de- or anti-icing system in aircraft structures. To investigate the long-term durability of heated GLARE previously reported thermal cycling tests up to 12,000 cycles are extended up to 144,000 cycles and moisture conditioning is included....
journal article 2019
document
Hagenbeek, M. (author), Sinke, J. (author)
Heated GLARE, a Fibre Metal Laminate with an integrated heater element, has been developed for de- or anti-icing systems in aircraft structures. Besides cyclic thermal loading these structures are also subjected to mechanical loading. To investigate the effect of static loading in addition to thermal cycling a series of tests have been performed...
journal article 2019
document
Hagenbeek, M. (author), Muller, B. (author), Sinke, J. (author)
By integrating heater elements in Fiber Metal Laminates, such as GLARE, the material has a promising potential as de- or anti-icing system in aircraft structures. Application of this so called "heated GLARE" material will however result in increase and (up to ten fold) more frequent temperature loading compares to the regular flight...
journal article 2018
document
Muller, B. (author), Hagenbeek, M. (author), Sinke, J. (author)
Fibre metal laminates with integrated heater elements have a promising potential as de- or anti-icing systems in aircraft structures. The alternating metal and composite lay-up in fibre metal laminates seems ideal for the development of a multifunctional skin with embedded heater elements. However, the long term durability needs to be carefully...
journal article 2016
Searched for: subject%3A%22shear%22
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