contributor author | S. R. Kidd | |
contributor author | M. A. Cherrett | |
contributor author | K. S. Chana | |
contributor author | J. S. Barton | |
contributor author | P. Meredith | |
contributor author | J. D. C. Jones | |
date accessioned | 2017-05-08T23:48:34Z | |
date available | 2017-05-08T23:48:34Z | |
date copyright | October, 1995 | |
date issued | 1995 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28646#635_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/116120 | |
description abstract | This paper describes the design, operation, construction, and demonstration of a new type of high-bandwidth unsteady temperature sensor based on fiber optics, and capable of operating in a high-speed multistage research compressor with flow representative of jet engine conditions. The sensing element is an optical coating of zinc selenide deposited on the end of an optical fiber. During evaluation in aerodynamic testing, a 1 K gas temperature resolution was demonstrated at 9.6 kHz and an upper bandwidth limit of 36 kHz achieved. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | A Fiber Optic Probe for Gas Total Temperature Measurement in Turbomachinery | |
type | Journal Paper | |
journal volume | 117 | |
journal issue | 4 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.2836582 | |
journal fristpage | 635 | |
journal lastpage | 641 | |
identifier eissn | 1528-8900 | |
keywords | Flow (Dynamics) | |
keywords | Temperature | |
keywords | Fibers | |
keywords | Temperature measurement | |
keywords | Compressors | |
keywords | Construction | |
keywords | Optical coatings | |
keywords | Resolution (Optics) | |
keywords | Design | |
keywords | Testing | |
keywords | Jet engines | |
keywords | Optical fiber | |
keywords | Probes | |
keywords | Temperature sensors AND Turbomachinery | |
tree | Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 004 | |
contenttype | Fulltext | |