CFD study of sting effects

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TypeTechnical Report
Series titleReport (Institute for Aerospace Research (Canada). Aerodynamics Laboratory); no. LTR-A-043
Physical description28 p.
AbstractA CFD study has been carried out to assess the sting mounting effect for the 1/16th scale model of the aurora aircraft. Two sting geometries at three angles of attack are studies. These studies indicate that sting geometry close to the fuselage does have a significant effect on the pressure distribution and that this effect is largely attributable to blockage caused by the sting.
Publication date
PublisherNational Research Council of Canada, Institute for Aerospace Research
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Peer reviewedNo
NPARC number21276131
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Record identifierbd347d67-d43d-468e-a42c-e63550d807bc
Record created2015-09-25
Record modified2016-10-03
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