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Emission analysis of a commercial aircraft for different ranges

Access

info:eu-repo/semantics/closedAccess

Date

2013

Author

Aydın, Hakan
Turan, Önder
Karakoç, T.Hikmet
Midilli, Adnan

Metadata

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Citation

Aydin, H., Turan, O., Karakoc, T. H., & Midilli, A. (2013). Emission analysis of a commercial aircraft for different ranges. In Causes, Impacts and Solutions to Global Warming (pp. 949-956). Springer New York. https://doi.org/10.4324/9781841505442

Abstract

In this chapter the lower take off cycle and total flight fuel consumptions and emissions of B737-400 commercial aircraft for selected routes are being calculated and evaluated for specified flight parameters. For case studies Eskisehir–Istanbul, Trabzon–Istanbul, and Ankara–London flights are selected as short-, medium-, and long-range flights with having 350, 980, and 3,270 km flight distances. The primary emissions released to environment are CO2, CH4, N2O, NOx, CO, and SO2. During Ankara–London flight with aircraft maximum takeoff weight operation (68,040 kg), B737-400 consumes 12,660 kg fuel and as a result 40,000 kg of CO2, 1.296 kg of CH4, 1.62 kg of N2O, 116.7 kg of NOx, 211.5 kg of CO, and 12.66 kg of SO2are emitted into environment. © Springer Science+Business Media New York 2013. All rights reserved.

Source

Causes, Impacts and Solutions to Global Warming

URI

https://doi.org/10.4324/9781841505442
https://hdl.handle.net/11436/4148

Collections

  • Makine Mühendisliği Bölümü Koleksiyonu [329]
  • Scopus İndeksli Yayınlar Koleksiyonu [5931]



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