Evaluation of the vortex generator flow control in the FOI-EIC-01 inlet at different flight conditions
2007 (English)In: Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2007, 687-701 p.Conference paper (Refereed)
The main goal of this work is to test the vortex generator flow control in the FOI-EIC-01 inlet at different flight conditions. The study has two phases. In the first, the entire flow around the UAV with inlet was calculated. Since it is not realistic to run RANS calculations of such a complicated configuration at a large number of flow conditions, the flow around the airframe-propulsion unit system was calculated as inviscid. The data on the boundaries of the inlet are collected and used in the second phase during tests of flow control.
Place, publisher, year, edition, pages
2007. 687-701 p.
Airframes, Flow control, Propulsion, Unmanned aerial vehicles (UAV)
IdentifiersURN: urn:nbn:se:kth:diva-6293ISBN: 978-156347903-8OAI: oai:DiVA.org:kth-6293DiVA: diva2:10969
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference; Cincinnati, OH; 8 July 2007 through 11 July 2007
QC 201009022006-10-252006-10-252010-09-02Bibliographically approved