liu.seSearch for publications in DiVA
Change search
ReferencesLink to record
Permanent link

Direct link
Validation of a numerical simulation tool for aircraft formation flight
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, The Institute of Technology.
2013 (English)In: Proceedings of the 4:th CEAS Conference in Linköping 2013 / [ed] Tomas Melin, Petter Krus, Emil Vinterhav, Knut Övrebö, 2013, 623-629 p.Conference paper (Other academic)
Abstract [en]

The use of formation flight for increased fuel efficiency has received a lot of attention in the last couple of years.This paper covers a numerical simulation of a NASA test flight utilizing a formation of two F18A Hornet aircraft. The numerical simulation was made using an adapted version of the vortex lattice method TORNADO, allowing for several aircraft to be simulated in a trimmed condition. The numerical results showed good agreement with the flight test data. Some discrepancies due to the numerical model not covering viscous diffusion was found as expected but not quantified or analyzed.

Place, publisher, year, edition, pages
2013. 623-629 p.
Keyword [en]
Formation flight, drag reduction, panel methods
National Category
Aerospace Engineering
URN: urn:nbn:se:liu:diva-106570ISBN: 978-91-7519-519-3OAI: diva2:716710
CEAS 2013 Air and Space Conference, 16-19 September 2013, Linköping, Sweden
Available from: 2014-05-12 Created: 2014-05-12 Last updated: 2014-06-16Bibliographically approved

Open Access in DiVA

Validation of a numerical simulation tool for aircraft formation flight.(844 kB)203 downloads
File information
File name FULLTEXT01.pdfFile size 844 kBChecksum SHA-512
Type fulltextMimetype application/pdf

Search in DiVA

By author/editor
Melin, Tomas
By organisation
Fluid and Mechatronic SystemsThe Institute of Technology
Aerospace Engineering

Search outside of DiVA

GoogleGoogle Scholar
Total: 203 downloads
The number of downloads is the sum of all downloads of full texts. It may include eg previous versions that are now no longer available

Total: 84 hits
ReferencesLink to record
Permanent link

Direct link