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Optical diagnostics for characterization of a full-size fighter-jet afterburner

Seyfried, Hans LU ; Särner, Gustaf LU ; Omrane, Alaa LU ; Richter, Mattias LU ; Schmidt, H and Aldén, Marcus LU (2005) ASME Turbo Expo 2005 - Gas Turbie Technology: Focus for the Future In Proceedings of the ASME Turbo Expo 2005 1. p.813-819
Abstract
In the present work the feasibility of using various optical/laser based techniques for characterization of the afterburner of a full-size aircraft engine have been investigated. The tests have been performed on-site at Volvo Aero Corporation and were mainly directed towards surface thermometry using thermographic phosphors and fuel visualization. All applications were studied for different engine running conditions, including various use of the afterburner (A/B). Laser-Induced Fluorescence (LIF) was employed for fuel visualization to investigate to what extent unburned fuel exits the afterburner. Laser-Induced Phosphorescence (LIP) from thermographic phosphors was used to measure two-dimensional surface temperatures on the outlet nozzle... (More)
In the present work the feasibility of using various optical/laser based techniques for characterization of the afterburner of a full-size aircraft engine have been investigated. The tests have been performed on-site at Volvo Aero Corporation and were mainly directed towards surface thermometry using thermographic phosphors and fuel visualization. All applications were studied for different engine running conditions, including various use of the afterburner (A/B). Laser-Induced Fluorescence (LIF) was employed for fuel visualization to investigate to what extent unburned fuel exits the afterburner. Laser-Induced Phosphorescence (LIP) from thermographic phosphors was used to measure two-dimensional surface temperatures on the outlet nozzle of the afterburner. In addition, the spectral characteristics of the burning jet stream were investigated. Copyright (Less)
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author
organization
publishing date
type
Chapter in Book/Report/Conference proceeding
publication status
published
subject
keywords
Surface thermometry, Jet streams, Fuel visualization
in
Proceedings of the ASME Turbo Expo 2005
volume
1
pages
813 - 819
publisher
American Society Of Mechanical Engineers (ASME)
conference name
ASME Turbo Expo 2005 - Gas Turbie Technology: Focus for the Future
external identifiers
  • WOS:000243375800091
  • Scopus:27744509749
ISBN
9780791846995
language
English
LU publication?
yes
id
02c0ee02-f86e-48f2-a1de-725aadc3c924 (old id 615364)
date added to LUP
2007-11-25 16:28:30
date last changed
2016-10-13 04:37:11
@misc{02c0ee02-f86e-48f2-a1de-725aadc3c924,
  abstract     = {In the present work the feasibility of using various optical/laser based techniques for characterization of the afterburner of a full-size aircraft engine have been investigated. The tests have been performed on-site at Volvo Aero Corporation and were mainly directed towards surface thermometry using thermographic phosphors and fuel visualization. All applications were studied for different engine running conditions, including various use of the afterburner (A/B). Laser-Induced Fluorescence (LIF) was employed for fuel visualization to investigate to what extent unburned fuel exits the afterburner. Laser-Induced Phosphorescence (LIP) from thermographic phosphors was used to measure two-dimensional surface temperatures on the outlet nozzle of the afterburner. In addition, the spectral characteristics of the burning jet stream were investigated. Copyright},
  author       = {Seyfried, Hans and Särner, Gustaf and Omrane, Alaa and Richter, Mattias and Schmidt, H and Aldén, Marcus},
  isbn         = {9780791846995},
  keyword      = {Surface thermometry,Jet streams,Fuel visualization},
  language     = {eng},
  pages        = {813--819},
  publisher    = {ARRAY(0xa172008)},
  series       = {Proceedings of the ASME Turbo Expo 2005},
  title        = {Optical diagnostics for characterization of a full-size fighter-jet afterburner},
  volume       = {1},
  year         = {2005},
}