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Validation of a numerical simulation tool for aircraft formation flight
Linköpings universitet, Institutionen för ekonomisk och industriell utveckling, Fluida och mekatroniska system. Linköpings universitet, Tekniska högskolan.
2013 (engelsk)Inngår i: Proceedings of the 4:th CEAS Conference in Linköping 2013 / [ed] Tomas Melin, Petter Krus, Emil Vinterhav, Knut Övrebö, 2013, s. 623-629Konferansepaper, Publicerat paper (Annet vitenskapelig)
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.

sted, utgiver, år, opplag, sider
2013. s. 623-629
Emneord [en]
Formation flight, drag reduction, panel methods
HSV kategori
Identifikatorer
URN: urn:nbn:se:liu:diva-106570ISBN: 978-91-7519-519-3 (tryckt)OAI: oai:DiVA.org:liu-106570DiVA, id: diva2:716710
Konferanse
CEAS 2013 Air and Space Conference, 16-19 September 2013, Linköping, Sweden
Tilgjengelig fra: 2014-05-12 Laget: 2014-05-12 Sist oppdatert: 2014-06-16bibliografisk kontrollert

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Validation of a numerical simulation tool for aircraft formation flight.(844 kB)317 nedlastinger
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Fil FULLTEXT01.pdfFilstørrelse 844 kBChecksum SHA-512
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Melin, Tomas

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Totalt: 317 nedlastinger
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