Real-time diagnostics of a jet engine exhaust using an intra-pulse quantum cascade laser spectrometer

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Duxbury, G. and Hay, K. G. and Langford, N. and Johnson, M. P. and Black, J. D. (2011) Real-time diagnostics of a jet engine exhaust using an intra-pulse quantum cascade laser spectrometer. Molecular Physics, 109 (17-18). pp. 2131-2142. ISSN 0026-8976 (https://doi.org/10.1080/00268976.2011.610367)

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Abstract

It has been demonstrated that an intra-pulse scanned quantum cascade laser spectrometer may be used to obtain real-time diagnostics of the amounts of carbon monoxide, carbon dioxide, and water, in the exhaust of an aero gas turbine (turbojet) engine operated in a sea level test cell. Measurements have been made of the rapid changes in composition following ignition, the composition under steady state operating conditions, and the composition changes across the exhaust plume. The minimum detection limit for CO in a double pass through a typical gas turbine plume of 50 cm in diameter, with 0.4 seconds integration time, is approximately 2 ppm.

ORCID iDs

Duxbury, G., Hay, K. G., Langford, N. ORCID logoORCID: https://orcid.org/0000-0002-3830-5542, Johnson, M. P. and Black, J. D.;
  • Item type:Article
    ID code:41554
    Dates:
    Date
    Event
    2011
    Published
    6 September 2011
    Published Online
    Subjects:Science > Physics
    Department:Faculty of Science > Physics
    Depositing user: Pure Administrator
    Date deposited:18 Oct 2012 14:59
    Last modified:11 Nov 2024 10:15
    Related URLs:
    URI:https://strathprints.strath.ac.uk/id/eprint/41554
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