Matches in SemOpenAlex for { <https://semopenalex.org/work/W2020062834> ?p ?o ?g. }
Showing items 1 to 63 of
63
with 100 items per page.
- W2020062834 abstract "Braided composites have good properties in mutually orthogonal directions, more balanced properties than traditional tape laminates, and have potentially better fatigue and impact resistance due to the interlacing. Another benefit is reduced manufacturing cost by reducing part count. Because of these potential benefits braided composites are being considered for various applications ranging from primary/secondary structures for aerospace structures [1]. These material systems are gaining popularity, in particular for the small business jets, where FAA requires taken off weights of 12,500 lb. or less. The new process, Vacuum Assisted Resin Transfer Molding (VARTM), is low cost, affordable and suitable for high volume manufacturing environment. Recently the aircraft industry has been successful in maufacturing wing flaps, using carbon fiber braids and epoxy resin and the VARTM process. To utilize these VARTM manufactured braided materials to the fullest advantage (and hence to avoid underutilization), it is necessary to understand their behavior under different loading and environmental conditions. This will reduce uncertainty and hence reduce the factor of safety in the design. Any typical structural member made of composite material is subjected to different types of loading such as static, impact, cyclic causing fatigue, and environmental effects such as change in temperature and exposure to moisture and other corrosives. It is well known that cyclic loading reduces the strength of a material and its useful life or, the fatigue strength of a material is lower than its static strength. This is true of all materials—metals, plastics, composite materials, etc. In structural applications, fatigue loading is unavoidable especially in aerospace and ground transportation applications. This research addresses the tensiontension fatigue behavior of biaxial braided composites." @default.
- W2020062834 created "2016-06-24" @default.
- W2020062834 creator A5024860385 @default.
- W2020062834 creator A5033762724 @default.
- W2020062834 date "2003-01-01" @default.
- W2020062834 modified "2023-09-23" @default.
- W2020062834 title "Fatigue Behavior of VARTM Manufactured Biaxial Braided Composites" @default.
- W2020062834 doi "https://doi.org/10.1115/imece2003-43850" @default.
- W2020062834 hasPublicationYear "2003" @default.
- W2020062834 type Work @default.
- W2020062834 sameAs 2020062834 @default.
- W2020062834 citedByCount "6" @default.
- W2020062834 countsByYear W20200628342013 @default.
- W2020062834 crossrefType "proceedings-article" @default.
- W2020062834 hasAuthorship W2020062834A5024860385 @default.
- W2020062834 hasAuthorship W2020062834A5033762724 @default.
- W2020062834 hasConcept C104779481 @default.
- W2020062834 hasConcept C124194741 @default.
- W2020062834 hasConcept C159985019 @default.
- W2020062834 hasConcept C166595027 @default.
- W2020062834 hasConcept C192562407 @default.
- W2020062834 hasConcept C2776656632 @default.
- W2020062834 hasConcept C2780566776 @default.
- W2020062834 hasConcept C33759916 @default.
- W2020062834 hasConcept C37696544 @default.
- W2020062834 hasConcept C76344452 @default.
- W2020062834 hasConceptScore W2020062834C104779481 @default.
- W2020062834 hasConceptScore W2020062834C124194741 @default.
- W2020062834 hasConceptScore W2020062834C159985019 @default.
- W2020062834 hasConceptScore W2020062834C166595027 @default.
- W2020062834 hasConceptScore W2020062834C192562407 @default.
- W2020062834 hasConceptScore W2020062834C2776656632 @default.
- W2020062834 hasConceptScore W2020062834C2780566776 @default.
- W2020062834 hasConceptScore W2020062834C33759916 @default.
- W2020062834 hasConceptScore W2020062834C37696544 @default.
- W2020062834 hasConceptScore W2020062834C76344452 @default.
- W2020062834 hasLocation W20200628341 @default.
- W2020062834 hasOpenAccess W2020062834 @default.
- W2020062834 hasPrimaryLocation W20200628341 @default.
- W2020062834 hasRelatedWork W145547448 @default.
- W2020062834 hasRelatedWork W1549729478 @default.
- W2020062834 hasRelatedWork W1592002519 @default.
- W2020062834 hasRelatedWork W1989939459 @default.
- W2020062834 hasRelatedWork W2071466705 @default.
- W2020062834 hasRelatedWork W2097438937 @default.
- W2020062834 hasRelatedWork W2182018370 @default.
- W2020062834 hasRelatedWork W2416151750 @default.
- W2020062834 hasRelatedWork W252091912 @default.
- W2020062834 hasRelatedWork W2587533324 @default.
- W2020062834 hasRelatedWork W2789381373 @default.
- W2020062834 hasRelatedWork W2803445489 @default.
- W2020062834 hasRelatedWork W2890433851 @default.
- W2020062834 hasRelatedWork W2953092857 @default.
- W2020062834 hasRelatedWork W3099076168 @default.
- W2020062834 hasRelatedWork W3199236626 @default.
- W2020062834 hasRelatedWork W572010183 @default.
- W2020062834 hasRelatedWork W641658048 @default.
- W2020062834 hasRelatedWork W767383267 @default.
- W2020062834 hasRelatedWork W781963219 @default.
- W2020062834 isParatext "false" @default.
- W2020062834 isRetracted "false" @default.
- W2020062834 magId "2020062834" @default.
- W2020062834 workType "article" @default.