Tests on a swept-back wing and body with endplates and wing tip tanks in the compressed air tunnel /
Salter, C.,author.
Jones, R.,author.
Weber, J.Comparison between the measured lift and drag and calculated values for the wing with tip tanks.
Great Britain.Her Majesty's Stationery Office.
Aeronautical Research Council (Great Britain),issuing body.
June 3, 1954.