Wind tunnel tests at Mach numbers up to 1.8 on a model with 1/36 scale wings and nacelles of a twin-engined supersonic aircraft (Bristol 188) /
Sutton, E. P.,author.
Hutton, P. G.,author.
Squire, L. C.,author.
Great Britain.Aeronautical Research Council,issuing body.
Great Britain.Her Majesty's Stationery Office.
"Feb. 1958. (23-9015-98)."