Propulsion Integration in an UAV

Marléne Johansson

24th AIAA Applied Aerodynamics Conference · 2006 · 24 citations · 11 references

Concepts

Abstract

This paper describes the work done in the project ”Propulsion Integration” at FOI, in which a propulsion system for an UAV has been designed and analyzed. Analyses have been carried out with CFD calculations, wind tunnel testing, calculations of structure dynamics and stealth properties. Final results from all disciplines are presented.

References

11