http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
experimental investigation of the transonic flow over an unswept wing of aspect ratio 3.5, taper ratio O. 5, with a 4 per cent biconvex section
Aeronautical Research Council (Great Britain)
Includes bibliographical references (page 11).
Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3209