Emission analysis of a commercial aircraft for different ranges

Hakan Aydin; Onder Turan; T. Hikmet Karakoc; Adnan Midilli

doi:10.4324/9781841505442

Emission analysis of a commercial aircraft for different ranges

Hakan Aydin, Onder Turan, T. Hikmet Karakoc, Adnan Midilli

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

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, NO_x, 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 NO_x, 211.5 kg of CO, and 12.66 kg of SO₂are emitted into environment.

Original language	English
Title of host publication	Causes, Impacts and Solutions to Global Warming
Publisher	Springer New York
Pages	949-956
Number of pages	8
ISBN (Electronic)	9781461475880
ISBN (Print)	9781461475873
DOIs	https://doi.org/10.4324/9781841505442
Publication status	Published - 1 Jan 2013
Externally published	Yes

Bibliographical note

Publisher Copyright:
© Springer Science+Business Media New York 2013. All rights reserved.

Keywords

Ankara
Emission
Emission analysis
Eskisehir
Flight
Green aircraft
Greenhouse gases
Istanbul
London
LTO cycle
Propulsion
Trabzon
Transportation

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

Access to Document

10.4324/9781841505442

Cite this

@inbook{ba02d38bb377480aa9f45b317692fa2d,

title = "Emission analysis of a commercial aircraft for different ranges",

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.",

keywords = "Ankara, Emission, Emission analysis, Eskisehir, Flight, Green aircraft, Greenhouse gases, Istanbul, London, LTO cycle, Propulsion, Trabzon, Transportation",

author = "Hakan Aydin and Onder Turan and Karakoc, {T. Hikmet} and Adnan Midilli",

year = "2013",

month = jan,

day = "1",

doi = "10.4324/9781841505442",

language = "English",

isbn = "9781461475873",

pages = "949--956",

booktitle = "Causes, Impacts and Solutions to Global Warming",

publisher = "Springer New York",

address = "United States",

}

TY - CHAP

T1 - Emission analysis of a commercial aircraft for different ranges

AU - Aydin, Hakan

AU - Turan, Onder

AU - Karakoc, T. Hikmet

AU - Midilli, Adnan

PY - 2013/1/1

Y1 - 2013/1/1

N2 - 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.

AB - 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.

KW - Ankara

KW - Emission

KW - Emission analysis

KW - Eskisehir

KW - Flight

KW - Green aircraft

KW - Greenhouse gases

KW - Istanbul

KW - London

KW - LTO cycle

KW - Propulsion

KW - Trabzon

KW - Transportation

UR - http://www.scopus.com/inward/record.url?scp=84949844897&partnerID=8YFLogxK

U2 - 10.4324/9781841505442

DO - 10.4324/9781841505442

M3 - Chapter

AN - SCOPUS:84949844897

SN - 9781461475873

SP - 949

EP - 956

BT - Causes, Impacts and Solutions to Global Warming

PB - Springer New York

ER -

Emission analysis of a commercial aircraft for different ranges

Abstract

Bibliographical note

Keywords

UN SDGs

Access to Document

Other files and links

Fingerprint

Cite this