Study on the performance of catalytic reactor for aircraft fuel tank inerting system

Author:

Peng XiaotianORCID,Qiu Doudou,Rui Ziliang,Feng ShiyuORCID,Peng Hao,Wang Chenchen

Publisher

Elsevier BV

Reference33 articles.

1. D.D. Dadia, Modeling wing tank flammability, Rutgers, the State University of, New Jersey, 2009, p. 10, https://search.proquest.com/docview/304993194.

2. D.E. Smith, Fuel tank inerting systems for civil aircraft, Colorado State University, Colorado, 2014, p. 32, https://search.proquest.com/docview/1651611871.

3. Effect of air supplementation on the performance of an onboard catalytic inerting system;Feng;Aerosp. Sci. Technol.,2019

4. H. Joseph. Service experience with liquid nitrogen fuel tank inerting system in FAA DC-9 aircraft, ADA000013, 1972, https://apps.dtic.mil/sti/citations/ADA000013.

5. I.A. Burch, S.R. Kennett, L. Fletcher, A risk assessment approach for selecting a replacement for halon 1301 fire suppressant, ADA391740, 2001. https://apps.dtic.mil/sti/citations/ADA391740.

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