Carbon-epoxy composites reinforced with nano-structures of tungsten disulfide for potential use in aircraft structures

Author:

Marjanović Milica,Simić Danica,Perković Srđa,Galović Jela,Burzić Zijah,Tasić Ana,Grga Slađan

Funder

Ministry of Education, Science and Technological Development of the Republic of Serbia

Publisher

Centre for Evaluation in Education and Science (CEON/CEES)

Reference22 articles.

1. JONES,R.M., Mechanics of Composite Materials, Second Edition, Taylor& Francis Inc., 1999.;

2. BAKER,A., DUTTON,S., KELLY,D.: Composite Materials for Aircraft Structures, SecondEdition, American Institute of Aeronautics and Astronautics. Inc, 2004.;

3. ILIĆ,I., ILIĆ,LJ., PERKOVIĆ,S., BLAZIĆ,М.: Strength Analysis Of Composite Structural Elements For Unmanned Aerial Vehicle, Fourth Serbian (29th Yu) Congress on Theoretical and Applied Mechanics, Vrnjačka banja, 4-7 Jun 2013, pp. 431-436;

4. MAKSIMOVIĆ,S., ILIĆ,I., GEORGIJEVIĆ,D., VASIĆ,Z., BOJANIĆ,М., STEFANOVIĆ,V.: Structural Analysis and Static Testing of a Tactical Unmanned Aerial Vechicle, ScientificTechnical Review, ISSN 1820-0206, 2013, Vol.63, No.2, pp. 58-62;

5. BRANTSEVA,T.V., SOLODILOV,V.I., ANTONOV,S.V., GORBUNOVA,I.Y., KOROHIN,R.A., SHAPAGIN,A.V., SMIRNOVA,N.M.: Epoxy modification with poly(vinyl acetate) and poly(vinyl butyral). I. Structure, thermal, and mechanical characteristics, J. APPL. POLYM. SCI. 2016, DOI: 10.1002/APP.44081;

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