Srihari, Shylaja and Revathi, A and Murugan, M. Sendil and Rao, RMVGK (2005) Environmental Conditioning Composites and Components for Aerospace and Allied Fields. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
The UPS and Grinder Units were subjected to low temperature test (i.e - 30°C/16hrs) in a low temperature/humidity chamber. After conditioning the units were handed over to the firm (i.e M/s Flotech Engineering Pvt Ltd for functional test. The smart Fatigue Meter unit were subjected to high temperature (i.e + 70°C/3hrs), low temperature (i.e - 40°C/4hrs) and thermal shock test (i.e - 40°C/1hr and + 70°C/l hr) in a temperature /humidity chamber. After conditioning the functional test was carried out by the ALD division, NAL. This document mainly brings out the details of the component /test specimens I conditioned and their test results
Item Type: | Monograph (Project Report) |
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Uncontrolled Keywords: | Grinder;UPS;Smart Fatigue meter;Glasslepoxy composite, Environmental tests |
Subjects: | AERONAUTICS > Aircraft Design, Testing & Performance CHEMISTRY AND MATERIALS > Composite Materials |
Depositing User: | Mr Nisanth |
Date Deposited: | 18 Nov 2011 05:03 |
Last Modified: | 18 Nov 2011 05:03 |
URI: | http://nal-ir.nal.res.in/id/eprint/10085 |
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