Thermodynamic analysis and preliminary design of the cooling system of a pulsejet for aeronautic propulsion TRANCOSSI, Michele, MOHAMMEDALAMIN, Omer, PASCOA, Jose and RODRIGUES, Frederico Available from Sheffield Hallam University Research Archive (SHURA) at: http://shura.shu.ac.uk/13960/ This document is the author deposited version. You are advised to consult the publisher's version if you wish to cite from it. Published version TRANCOSSI, Michele, MOHAMMEDALAMIN, Omer, PASCOA, Jose and RODRIGUES, Frederico (2016). Thermodynamic analysis and preliminary design of the cooling system of a pulsejet for aeronautic propulsion. International Journal of Heat and Technology, 34 (2), S528-S534. Copyright and re-use policy See http://shura.shu.ac.uk/information.html Sheffield Hallam University Research Archive http://shura.shu.ac.uk INTERNATIONAL JOURNAL OF A publication of IIETA HEAT AND TECHNOLOGY ISSN: 0392-8764 Vol. 34, Special Issue 2, October 2016, pp. S528-S534 DOI: https://doi.org/10.18280/ijht.34S247 Licensed under CC BY-NC 4.0 http://www.iieta.org/Journals/IJHT Thermodynamic Analysis and Preliminary Design of the Cooling System of a Pulsejet for Aeronautic Propulsion Michele Trancossi 1*, Omer Mohammedalamin 2, Jose C. Pascoa 3 and Frederico Rodrigues 3 1 Material and Engineering Research Insitute, ACES, Sheffield Hallam University, City Campus, Howard Street, Sheffield S1 1WB, UK, 2 Faculty of Arts, Computing, Engineering and Sciences, Sheffield Hallam University, City Campus, Howard Street, Sheffield S1 1WB, UK 3 Center for Mechanical and Aerospace Science and Technology, Universitade da Beira Interior, 6200-Covilhã, PT Email:
[email protected] ABSTRACT This paper is a preliminary step through an effective redesign of valved pulsejet.