Senthil Kumar, P and Jayasankar, S and Satisha, Vishwanath and Sateesh, VL and Kamaleshaiah, MS and Dayananda, GN (2013) Development and wind tunnel evaluation of an SMA based trim tab actuator for a civil aircraft. SMART MATERIALS AND STRUCTURES, 22 (9).
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Official URL: http://iopscience.iop.org/
Abstract
This paper presents the development and wind tunnel evaluation of an SMA based smart trim tab for a typical two seater civil aircraft. The SMA actuator was housed in the port side of the elevator for the purpose of actuating the trim tab. Wind tunnel tests were conducted on a full scale horizontal tail model with elevator and trim tab at free stream speeds of 25, 35 and 45 m s
| Item Type: | Article |
|---|---|
| Subjects: | AERONAUTICS > Research and Support Facilities (Air) |
| Depositing User: | Mr Satisha |
| Date Deposited: | 02 Jan 2014 10:23 |
| Last Modified: | 13 Aug 2015 10:04 |
| URI: | http://nal-ir.nal.res.in/id/eprint/11885 |
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