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2013 | OriginalPaper | Chapter

14. Applications of Infrared Technology to Helicopter Flight Testing

Author : Laurent Girard

Published in: Advanced In-Flight Measurement Techniques

Publisher: Springer Berlin Heidelberg

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Abstract

This chapter deals with some applications of the infrared technology for industrial flight tests of helicopters. The main application concerns the measurement of structural temperature. Flight tests are performed on a prototype helicopter equipped with suitable infrared cameras in order to measure the surface temperature of structures located in the vicinity of the engines exhaust nozzles. These trials show that the infrared technology is fully usable for helicopter flight testing purposes and the results inferred underline that this instrumentation offers clear advantages compared with the methods generally used.

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Literature
1.
go back to reference K. de Groot, U. Fey, Y. Le Sant, in Thermography as a Tool in Wind Tunnel Testing (D2.10), European Windtunnel Association, European Commission 6th Framework Programme, March 2006 K. de Groot, U. Fey, Y. Le Sant, in Thermography as a Tool in Wind Tunnel Testing (D2.10), European Windtunnel Association, European Commission 6th Framework Programme, March 2006
Metadata
Title
Applications of Infrared Technology to Helicopter Flight Testing
Author
Laurent Girard
Copyright Year
2013
Publisher
Springer Berlin Heidelberg
DOI
https://doi.org/10.1007/978-3-642-34738-2_14

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