Optical diagnostics for characterization of a full-size fighter-jet afterburner
(2005) ASME Turbo Expo 2005 - Gas Turbie Technology: Focus for the Future 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)
Please use this url to cite or link to this publication:
https://lup.lub.lu.se/record/615364
- author
- Seyfried, Hans LU ; Särner, Gustaf LU ; Omrane, Alaa LU ; Richter, Mattias LU ; Schmidt, H and Aldén, Marcus LU
- organization
- publishing date
- 2005
- type
- Chapter in Book/Report/Conference proceeding
- publication status
- published
- subject
- keywords
- Surface thermometry, Jet streams, Fuel visualization
- host publication
- 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
- conference location
- Reno-Tahoe, NV, United States
- conference dates
- 2005-06-06 - 2005-06-09
- 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
- 2016-04-04 09:58:04
- date last changed
- 2022-01-29 19:32:06
@inproceedings{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}}, booktitle = {{Proceedings of the ASME Turbo Expo 2005}}, isbn = {{9780791846995}}, keywords = {{Surface thermometry; Jet streams; Fuel visualization}}, language = {{eng}}, pages = {{813--819}}, publisher = {{American Society Of Mechanical Engineers (ASME)}}, title = {{Optical diagnostics for characterization of a full-size fighter-jet afterburner}}, volume = {{1}}, year = {{2005}}, }