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Author
Hamins, A. | Baghdadi, D. | Borthwick, P. | Glover, M. P. | Grosshandler, W. L. | Lowe, D. L. | Melton, L. | Presser, C.
Title
Suppression of Simulated Engine Nacelle Fires.
Coporate
National Institute of Standards and Technology, Gaithersburg, MD University of Texas, Dallas
Report
NISTIR 5499, September 1994,
Book or Conf
National Institute of Standards and Technology. Annual Conference on Fire Research: BOOK OF ABSTRACTS. October 17-20, 1994, Gaithersburg, MD, 7-8 p., 1994
Keywords
fire research | nacelle fires | extinguishment | aircraft fires
Abstract
The engine nacelle encases the jet engine compressor, combustor and turbine. A nacelle fire is typically a turbulent diffusion flame stabilized behind an obstruction in a moderately high speed air flow. The most likely source for a fire in the nacelle are leaks in the fuel lines carrying jet fuel or hydraulic fluid, that can feed the fire either as a spray or as a pre-vaporized gas. Temperatures as high as 150 deg C are common in normal operating engine nacelles.