FoT25 2003-2005: Propulsion integration - final report

Authors:

  • Johansson Marlene (ed)

Publish date: 2006-01-01

Report number: FOI-R--2017--SE

Pages: 40

Written in: English

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Abstract

This report summarizes the work done in the FoT25-project "Propulsion Integration". A propulsion system for an UAV has been designed and analyzed, where the main focus has been the inlet. Analysis has been carried out with CFD calculations, wind tunnel testing, calculation of fluid-structure interactions and stealth properties.