Wind tunnel test on a 1/12th scale model of the Bristol Type 188 research aircraft with rectangular, wedge intakes at Mach numbers from 2.0 to 2.7 /
Cook, T. A.,author.
Great Britain.Aeronautical Research Council,issuing body.
Great Britain.Her Majesty's Stationery Office.
"April 1963. (23-9016-17)."