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contributor authorKedir, Nesredin
contributor authorFaucett, David
contributor authorSanchez, Luis
contributor authorChoi, Sung R.
date accessioned2017-11-25T07:21:23Z
date available2017-11-25T07:21:23Z
date copyright2016/20/9
date issued2017
identifier issn0742-4795
identifier othergtp_139_02_021301.pdf
identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4237036
description abstractForeign object damage (FOD) behavior of an N720/alumina oxide/oxide ceramic matrix composite (CMC) was characterized at ambient temperature by using spherical projectiles impacted at velocities ranging from 100 to 350 m/s. The CMC targets were subject to ballistic impact at a normal incidence angle while being loaded under different levels of tensile loading in order to simulate conditions of rotating aeroengine airfoils. The impact damage of frontal and back surfaces was assessed with respect to impact velocity and load factor. Subsequent postimpact residual strength was also estimated to determine quantitatively the severity of impact damage. Impact force was predicted based on the principles of energy conservation.
publisherThe American Society of Mechanical Engineers (ASME)
titleForeign Object Damage in an Oxide/Oxide Ceramic Matrix Composite Under Prescribed Tensile Loading
typeJournal Paper
journal volume139
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4034360
journal fristpage21301
journal lastpage021301-8
treeJournal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 002
contenttypeFulltext


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