liu.seSearch for publications in DiVA
Operational message
There are currently operational disruptions. Troubleshooting is in progress.
Change search
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • oxford
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf
Cool Planes for Hot Missions: Early but Effective Aircraft Thermal Management Design
Saab AB, Linköping, Sweden.
Linköping University, Department of Management and Engineering, Product Realisation. Linköping University, Faculty of Science & Engineering.ORCID iD: 0000-0002-7210-0209
Technical University of Braunschweig, Germany.ORCID iD: 0000-0002-7797-4239
2024 (English)In: AIAA Aviation Forum and ASCEND co-located Conference Proceedings, American Institute of Aeronautics and Astronautics, 2024Conference paper, Published paper (Refereed)
Abstract [en]

Multi-role fighter aircraft are facilitated by operational and platform capabilities that are in turn supported by basic aircraft function. Thermal management (TM) is a basic aircraft function. Effective TM design at the aircraft concept stage can determine if it can support the intended operational and aircraft capabilities early in the aircraft project. In this study, a three-session workshop with a cross-functional team for TM design was conducted at Saab AB. The outcomes from the workshop resulted in a framework for a detailed understanding of the steps to be carried out iteratively for TM design by a cross-functional team. It also provides the dependencies for these steps and the various functional groups that need to be involved in each step. The steps can be used to iterate TM design at the aircraft concept stage and understand the implications on aircraft and operational capabilities. Further, the workshop methodology presented can be used to obtain similar frameworks for design of other basic functions at the aircraft concept stage.

Place, publisher, year, edition, pages
American Institute of Aeronautics and Astronautics, 2024.
National Category
Vehicle and Aerospace Engineering
Identifiers
URN: urn:nbn:se:liu:diva-210938DOI: 10.2514/6.2024-4556ISI: 001397464102063Scopus ID: 2-s2.0-85204216512ISBN: 9781624107160 (print)OAI: oai:DiVA.org:liu-210938DiVA, id: diva2:1927464
Conference
AIAA Aviation Forum and ASCEND, Las Vegas, 29 July - 2 August, 2024
Funder
Vinnova
Note

Funding Agencies|VINNOVA (The Swedish Governmental Agency for Innovation Systems)

Available from: 2025-01-15 Created: 2025-01-15 Last updated: 2025-03-05Bibliographically approved

Open Access in DiVA

No full text in DiVA

Other links

Publisher's full textScopus

Authority records

Drego, AdeliaWiberg, AntonStaack, Ingo

Search in DiVA

By author/editor
Drego, AdeliaWiberg, AntonStaack, Ingo
By organisation
Product RealisationFaculty of Science & Engineering
Vehicle and Aerospace Engineering

Search outside of DiVA

GoogleGoogle Scholar

doi
isbn
urn-nbn

Altmetric score

doi
isbn
urn-nbn
Total: 150 hits
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • oxford
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf