Low-speed wind-tunnel tests on an unswept wing-fuselage model of aspect Ratio 9.8, with tangential blowing over trailing-edge flaps and ailerons, including the effect of slipstream.
Lawford, J. A.,author.
Great Britain.Ministry of Aviation Supply,issuing body.
Great Britain.Her Majesty's Stationery Office.
Aeronautical Research Council (Great Britain)