Structural Evaluation of Exoskeletal Engine Fan Blades
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1861
Reference5 articles.
1. Abumeri, G.H. and Chamis, C. C. "EST/BEST: a Computer Code for Assessing the Benefits of Advanced Aerospace Technologies", published in the journal of Advances in Engineering Software,1997 Elsevier Science Limited, Printed in Great Britain.,pp.231-238.
2. Composite structure global fracture toughness via computational simulation
3. Kuguoglu, L., Abumeri, G.H., and Chamis, C. C."Durability and Damage Tolerance: Comparative Evaluation of Metallic and Composite Fan Blades", AIAA Paper 2002-1527, 43STAIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference,April232002,Denver,COTable I. FanBladeDesignParameters
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1. Optimal design method for composite blades using stiffness weights;Composite Structures;2020-04
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