Design, manufacturing and operation of a small turbojet-engine for research purposes
A research project is on going, at the University of Padova, to develop a 200Â N static-thrust engine to be used for both didactic and research activities. This paper describes in detail all the phases required to set-up such an engine, including design, manufacturing and operation. The jet engine features a single-stage centrifugal compressor developing 2.66:1 compression ratio at 60,000Â rpm, a direct-flow annular combustion chamber and a single-stage axial turbine with 950Â K turbine-inlet temperature (TIT). All the design and manufacturing details are provided, as well as the operation procedure together with experimental results.
Volume (Year): 84 (2007)
Issue (Month): 11 (November)
|Contact details of provider:|| Web page: http://www.elsevier.com/wps/find/journaldescription.cws_home/405891/description#description|
|Order Information:|| Postal: http://www.elsevier.com/wps/find/journaldescription.cws_home/405891/bibliographic|
When requesting a correction, please mention this item's handle: RePEc:eee:appene:v:84:y:2007:i:11:p:1102-1116. See general information about how to correct material in RePEc.
For technical questions regarding this item, or to correct its authors, title, abstract, bibliographic or download information, contact: (Zhang, Lei)
If references are entirely missing, you can add them using this form.