Cahill, P. (1996). The Development of a Flammability Test Method for Aircraft Blankets (Report No. DOT/FAA/AR-96/15). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://doi.org/10.21949/1404594
Cahill, Patricia. The Development of a Flammability Test Method for Aircraft Blankets. Report no. DOT/FAA/AR-96/15. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996. https://doi.org/10.21949/1404594.
Cahill, Patricia The Development of a Flammability Test Method for Aircraft Blankets. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996, Report no. DOT/FAA/AR-96/15, ROSA P. https://doi.org/10.21949/1404594.
Flammability testing of aircraft blankets was conducted in order to develop a fire performance test method and performance criteria for blankets supplied to commercial aircraft operators. Aircraft blankets were subjected to vertical Bunsen burner testing, 4-ply vertical testing, full-scale match and cigarette testing, and single- and 4-ply horizontal testing. It was found that the 4-ply horizontal test correlates well with the full-scale match tests, produces consistent test results, and realistically evaluates ease of ignition.
Cahill, P. (1996). The Development of a Flammability Test Method for Aircraft Blankets (Report No. DOT/FAA/AR-96/15). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://doi.org/10.21949/1404594
Cahill, Patricia. The Development of a Flammability Test Method for Aircraft Blankets. Report no. DOT/FAA/AR-96/15. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996. https://doi.org/10.21949/1404594.
Cahill, Patricia The Development of a Flammability Test Method for Aircraft Blankets. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996, Report no. DOT/FAA/AR-96/15, ROSA P. https://doi.org/10.21949/1404594.
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