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  4. Minimizing the climate impact of the next generation aircraft using novel climate functions for aircraft design
 
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Minimizing the climate impact of the next generation aircraft using novel climate functions for aircraft design

Publikationstyp
Conference Paper
Date Issued
2022-01-01
Sprache
English
Author(s)
Radhakrishnan, Kaushik 
Lufttransportsysteme M-28  
Deck, K.  
Proesmans, Pieter-Jan  
Linke, Florian  
Yin, Feijia  
Grewe, Volker  
Lührs, Benjamin 
Vos, Roelof  
Niklaß, Malte  
Dedoussi, Irene  
Institut
Lufttransportsysteme M-28  
TORE-URI
http://hdl.handle.net/11420/15417
Volume
1
Start Page
549
End Page
566
Citation
33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022 1: 549 - 566 (2022)
Contribution to Conference
33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022  
Publisher Link
https://www.icas.org/ICAS_ARCHIVE/ICAS2022/data/papers/ICAS2022_0602_paper.pdf
Scopus ID
2-s2.0-85159696026
Publisher
Curran
ISBN
978-1-7138-7116-3
ISBN of container
978-171387116-3
The aircraft’s environmental performance on fleet level is so far completely decoupled from the design process. The climate impact from aviation arising from non-CO2 effects are largely independent from CO2 emissions, but rather depend on the atmospheric state. Previously complex climate-chemistry models were used to evaluate the non-CO2 emissions impact on climate. This is far too computationally demanding for a multidisciplinary design optimisation (MDO) process, requiring a multitude of climate impact evaluations. The question then is, how to efficiently design the next generation climate optimal aircraft? In this paper, a new concept for designing aircraft with minimum climate impact using Climate Functions for Aircraft Design (CFAD) is presented. The content of this paper provides an overview of the development of these innovative CFAD and demonstrates the ability to be integrated in an existing MDO framework. The mitigation potential by optimising aircraft design using CFAD is analysed with respect to different cruise conditions and by minimizing the overall climate impact. To validate the CFAD, a higher fidelity assessment is carried out. Finally, the key performance indicators, i.e. fuel consumption, flight time and operating cost, of the optimised aircraft design are compared to that of the reference aircraft.
Subjects
Aircraft design
CFAD
Climate functions
Climate impact
Multidisciplinary design optimisation
DDC Class
600: Technik
620: Ingenieurwissenschaften
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