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An avian modeling approach for analyzing bone loss due to disuse

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dc.contributor.author Foutz, TL en
dc.contributor.author Rowland, GN en
dc.contributor.author Evans, M en
dc.date.accessioned 2014-06-06T06:43:14Z
dc.date.available 2014-06-06T06:43:14Z
dc.date.issued 1997 en
dc.identifier.issn 00012351 en
dc.identifier.uri http://62.217.125.90/xmlui/handle/123456789/1113
dc.relation.uri http://www.scopus.com/inward/record.url?eid=2-s2.0-0031280371&partnerID=40&md5=7cc6fdbb387f3124b254420d672a3fbe en
dc.subject Biomechanics en
dc.subject Bone en
dc.subject Osteopenia en
dc.subject Pullet en
dc.subject.other Biomechanics en
dc.subject.other Medical problems en
dc.subject.other Nondestructive examination en
dc.subject.other Orthopedics en
dc.subject.other Physiological models en
dc.subject.other Bone loss en
dc.subject.other Bone mass en
dc.subject.other Osteopenia en
dc.subject.other Pullet en
dc.subject.other Bone en
dc.title An avian modeling approach for analyzing bone loss due to disuse en
heal.type journalArticle en
heal.publicationDate 1997 en
heal.abstract Osteopenia has been a major skeletal problem of leghorns in production. Mechanical usage has been considered a major factor in controlling ultimate bone mass. A disuse model was characterized over a 35 day period in pullets to determine the sequential temporal change in lamellar cortical bone of the wing. Ulna cortical bone area was decreased at all four time intervals in the immobilized wings. At 21 days post-immobilization, the cortical bone area was decreased most significantly. Osteoblastic activity was most consistently altered by immobilization on the posterior quadrant of the ulna. Cortical endosteal eroded surface was significantly increased on day 14 in experiment 1 and day 28 in experiment 2. Nondestructive material testing indicated that a 30% to 40% reduction in stiffness for the immobilized wing.Osteopenia has been a major skeletal problem of leghorns in production. Mechanical usage has been considered a major factor in controlling ultimate bone mass. A disuse model was characterized over a 35 day period in pullets to determine the sequential temporal change in lamellar cortical bone of the wing. Ulna cortical bone area was decreased at all four time intervals in the immobilized wings. At 21 days post-immobilization, the cortical bone area was decreased most significantly. Osteoblastic activity was most consistently altered by immobilization on the posterior quadrant of the ulna. Cortical endosteal eroded surface was significantly increased on day 14 in experiment 1 and day 28 in experiment 2. Nondestructive material testing indicated that a 30% to 40% reduction in stiffness for the immobilized wing. en
heal.publisher ASAE, St. Joseph, MI, United States en
heal.journalName Transactions of the American Society of Agricultural Engineers en
dc.identifier.issue 6 en
dc.identifier.volume 40 en
dc.identifier.spage 1719 en
dc.identifier.epage 1725 en


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