Comparative Analysis of Inerting Effects of Open and Closed Vent Systems Fuel Tanks
Author:
Funder
National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s42405-024-00791-9.pdf
Reference24 articles.
1. Langton R, Clark C, Hewitt M et al (2009) Aircraft fuel systems. Wiley, Chichester, UK, p 235
2. Pei Y, Shi B (2016) Method for analyzing the effect of projectile impact on aircraft fuel tank inerting for survivability design. J Aerosp Eng 230(13):2345–2355. https://doi.org/10.1177/0954410015623573
3. Gupta A (2009) Method and system for making a fuel-tank inert without an inert gas. SAE Int J Aerosp 2(1):75–82. https://doi.org/10.4271/2009-01-3134
4. Cavage WM (2005) The effect of fuel on an inert ullage in a commercial transport airplane fuel tank. Federal Aviation Administration, DOT/FAA/AR-05/25. https://www.fire.tc.faa.gov/pdf/05-25.pdf
5. Summer SM (2002) Limiting oxygen concentration required to inert jet fuel vapors existing at reduced fuel tank pressures. Federal Aviation Administration, DOT/FAA/AR-TN02/79. https://www.fire.tc.faa.gov/pdf/TN02-79.pdf
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