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Aircraft conceptual design for optimal environmental performance

Part of: Sustainable Aerospace

Published online by Cambridge University Press:  27 January 2016

R. P. Henderson ,
J. R. R. A. Martins  and
R. E. Perez
R. P. Henderson
Affiliation:
Institute for Aerospace Studies, University of Toronto, Ontario, Canada
J. R. R. A. Martins*
Affiliation:
Department of Aerospace Engineering, University of Michigan, Michigan, USA
R. E. Perez
Affiliation:
Department of Mechanical and Aerospace Engineering, Royal Military College of Canada, Kingston, Ontario, Canada
*
jrram@umich.edu
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Abstract

Consideration of the environmental impact of aircraft has become critical in commercial aviation. The continued growth of air traffic has caused increasing demands to reduce aircraft emissions, imposing new constraints on the design and development of future airplane concepts. In this paper, an aircraft design optimisation framework is used to design aircraft that minimise specific environmental metrics. Multidisciplinary design optimisation is used to optimise aircraft by simultaneously considering airframe, engine and mission. The environmental metrics considered in this investigation are CO2 emissions — which are proportional to fuel burn — and landing-takeoff NOx emissions. The results are compared to those of an aircraft with minimum direct operating cost. The design variables considered in the optimisation problems include aircraft geometry, engine parameters, and cruise settings. An augmented Lagrangian particle swarm optimiser and a genetic algorithm are used to solve the single objective and multi-objective optimisation problems, respectively.

Type
Research Article
Information
The Aeronautical Journal , Volume 116 , Issue 1175 , January 2012 , pp. 1 - 22
Copyright
Copyright © Royal Aeronautical Society 2012 

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