Development of reliable modeling methodologies for fan blade out containment analysis – Part I: Experimental studies-Reference-Cited by-同舟云学术

Development of reliable modeling methodologies for fan blade out containment analysis – Part I: Experimental studies

Published:2009-01 Issue:1 Volume:36 Page:1-11
ISSN:0734-743X
Container-title:International Journal of Impact Engineering
language:en
Short-container-title:International Journal of Impact Engineering

Author:

Naik D.,Sankaran S.,Mobasher B.,Rajan S.D.,Pereira J.M.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Safety, Risk, Reliability and Quality,Aerospace Engineering,Automotive Engineering,Civil and Structural Engineering

Reference10 articles.

1. Modeling of multi-layer composite fabrics for gas turbine engine containment systems;Sharda;ASCE J Aerosp Eng,2006

2. Explicit FEA modeling of multi-layer composite fabric for gas turbine engines containment systems;DOT/FAA/AR-04/40, P1–P4,2005

3. Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems. Part 2: ballistic impact testing;Pereira,2004

4. Stahlecker Z, Mobasher B, Rajan SD, Pereira JM. Development of reliable modeling methodologies for engine fan blade out containment analysis. Part II: finite element analysis; Int J Impact Eng, in press.

5. Mechanical properties of Kevlar KM2 single fiber;Cheng;J Mater Eng Technol,2005

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