Fracture Probability Accumulation As Damage Accumulation in Lifetime and Crack Propagation for Dynamically Loaded Aircraft Sheet Metal. [BRUCHWAHRSCHEINLICHKEITSAKKUMULATION ALS SCHADENS-AKKUMULATION ZUR LEBENSDAUER- UND RISSFORTSCHRITTSVORHERSAGE DYNAMISCH BEANSPRUCHTER LUFTFAHRTBLECHE.]

Makris, P; Stein, K

dc.contributor.author	Makris, P	en
dc.contributor.author	Stein, K	en
dc.date.accessioned	2014-03-01T01:38:38Z
dc.date.available	2014-03-01T01:38:38Z
dc.date.issued	1984	en
dc.identifier.issn	00255300	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/22302
dc.relation.uri	http://www.scopus.com/inward/record.url?eid=2-s2.0-0021504731&partnerID=40&md5=05018a03c7068692439eaf5dedaa047e	en
dc.subject.other	FRACTURE MECHANICS - Theory	en
dc.subject.other	METALS TESTING - Fatigue	en
dc.subject.other	PROBABILITY - Random Processes	en
dc.subject.other	SHEET AND STRIP METAL	en
dc.title	Fracture Probability Accumulation As Damage Accumulation in Lifetime and Crack Propagation for Dynamically Loaded Aircraft Sheet Metal. [BRUCHWAHRSCHEINLICHKEITSAKKUMULATION ALS SCHADENS-AKKUMULATION ZUR LEBENSDAUER- UND RISSFORTSCHRITTSVORHERSAGE DYNAMISCH BEANSPRUCHTER LUFTFAHRTBLECHE.]	en
heal.type	journalArticle	en
heal.publicationDate	1984	en
heal.abstract	A method is presented by means of which the crack propagation and lifetime of dynamically loaded aircraft sheet metal can be predicted with the aid of an engineering model by employing stochastic fracture probability concepts. The model is based on the assumption that the material consists of very small elastic particles which under dynamic loading show a corresponding fracture probability and pass directly (i. e. , without causing partial damage) from the unfractured to the fractured state.	en
heal.journalName	Materialpruefung/Materials Testing	en
dc.identifier.volume	26	en
dc.identifier.issue	10	en
dc.identifier.spage	349	en
dc.identifier.epage	353	en