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Global-Warming-Optimized Aircraft Design

PROJECTS
Funding
European
European Union
Duration
-
Status
Ongoing
Geo-spatial type
Other
Total project cost
€917 500
EU Contribution
€915 250
Project Acronym
GLOWOPT
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Environmental/Emissions aspects
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP09-2018-02
Link to CORDIS
Objectives

The high-level objective of the proposed GLOWOPT project is the development and validation of Climate Cost Functions (CCFs) with respect to minimizing global warming and their application to the multidisciplinary design optimization of next-generation aircraft for relevant market segments.

Several objectives are set in order to reach this target. The first objective is to provide an overview of the state of the art on the scientific background of the relation between aircraft design and operation and its climate impact.

The second objective is to derive characteristic aircraft design requirements, primarily payload and range, based on statistical data analysis of the worldwide aircraft fleet and route structure for future entries into Service using a comprehensive air traffic forecast model.

The third objective is to develop climate cost functions for the use in the aircraft design optimisation, which reliably represent the climate impact of CO2, NOx, H2O emissions, as well as contrail-cirrus effects.

The fourth objective is to perform a Multidisciplinary Design Optimization with respect to the climate cost function to find a set of operational parameters, design parameters and aircraft technologies that minimize the climate impact of the aircraft design using an existing MDO environment that applies the developed CCFs as objective function.

The fifth and final objective is to perform an assessment of the aircraft designs chosen in order to quantify their impact on important metrics such as landing and take-off noise, emissions and cash operating cost. For this purpose, a higher-fidelity simulation integrating existing flight performance, emission and climate impact models is adapted and applied to simulate the aircraft design solution in an operational environment.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.5.10.
Other Programme
JTI-CS2-2018-CFP09-THT-04 Aircraft Design Optimisation providing optimum performance towards limiting aviation’s contribution towards Global Warming

Partners

Lead Organisation
Organisation
Technische Universitat Hamburg
Address
Am Schwarzenberg Campus 1, 21073 Hamburg, Germany
Organisation website
EU Contribution
€334 625
Partner Organisations
Organisation
Technische Universiteit Delft
Address
STEVINWEG 1, 2628 CN DELFT, Netherlands
Organisation website
EU Contribution
€580 625

Technologies

Technology Theme
Aircraft design and manufacturing
Technology
Aircraft design model
Development phase
Research/Invention

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