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International Journal of Aerospace Engineering
Volume 2016, Article ID 8913901, 9 pages
http://dx.doi.org/10.1155/2016/8913901
Research Article

Effects of Duct Cross Section Camber and Thickness on the Performance of Ducted Propulsion Systems for Aeronautical Applications

Dipartimento di Ingegneria Industriale, Università degli Studi di Napoli Federico II, Via Claudio 21, 80125 Napoli, Italy

Received 11 August 2015; Revised 18 January 2016; Accepted 19 January 2016

Academic Editor: Christopher J. Damaren

Copyright © 2016 Rodolfo Bontempo and Marcello Manna. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

How to Cite this Article

Rodolfo Bontempo and Marcello Manna, “Effects of Duct Cross Section Camber and Thickness on the Performance of Ducted Propulsion Systems for Aeronautical Applications,” International Journal of Aerospace Engineering, vol. 2016, Article ID 8913901, 9 pages, 2016. https://doi.org/10.1155/2016/8913901.