NASA NTRS ยท 19810015645
Development of advanced lightweight containment systems
Abstract
Parametric type data were obtained on advanced lightweight containment systems. These data were used to generate design methods and procedures necessary for the successful development of such systems. The methods were then demonstrated through the design of a lightweight containment system for a CF6 size engine. The containment concept evaluated consisted basically of a lightweight structural sandwich shell wrapped with dry Kevlar cloth. The initial testing was directed towards the determination of the amount of Kevlar required to result in threshold containment for a specific set of test conditions. A relationship was then developed between the thickness required and the energy of the released blade so that the data could be used to design for conditions other than those tested.
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Stotler, C.. 1981-05-01. Development of advanced lightweight containment systems. https://ntrs.nasa.gov/citations/19810015645
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