National Research Council of Canada. NRC Institute for Aerospace Research
Text, Technical Report
A 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.
National Research Council of Canada. Institute for Aerospace Research
Laboratory Technical Report (National Research Council of Canada. Institute for Aerospace Research), no. LTR-A-043 (September 1999).