| dc.contributor.advisor | Papadakis, Michael | |
| dc.contributor.author | Bikkannavar, Karan Vishwanath | |
| dc.date.accessioned | 2016-11-14T21:53:49Z | |
| dc.date.available | 2016-11-14T21:53:49Z | |
| dc.date.issued | 2016-05 | |
| dc.identifier.other | t16002 | |
| dc.identifier.uri | http://hdl.handle.net/10057/12647 | |
| dc.description | Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering | |
| dc.description.abstract | The new trend in aviation industry is towards „all electric aircraft‟. Thus, there‟s a strong
desire to replace bleed air systems with efficient electrical ice protection systems that would
provide adequate ice protection.
In the current thesis study, a computational methodology was developed to support the
design and assess the performance of electro-thermal ice protection systems (ETIPS) for de-icing
fixed wing aircraft. The methodology developed was tested using a range of geometries and
electrical heater configurations and was validated with experimental data obtained by researchers
at Wichita State University (WSU) and other organizations. | |
| dc.format.extent | xiv, 98 p. | |
| dc.language.iso | en_US | |
| dc.publisher | Wichita State University | |
| dc.rights | Copyright 2016 Karan Vishwanath Bikkannavar | |
| dc.subject.lcsh | Electronic dissertations | |
| dc.title | Computational methodology for electro-thermal ice protection system analysis | |
| dc.type | Thesis | |
