Wind tunnel measurements of the lift-dependent drag of thin conically cambered slender Delta wings at Mach numbers 1.4 and 1.8
By: M. S. Igglesden.
Contributors: Aeronautical Research Council (Great Britain)
Series: Aeronautical Research Council.  Current papers -- no. 519
Publisher: Ministry of Aviation, Aeronautical Research Council
Published: 1960
Place of publication: London
Number of pages: 22
Notes: Also published as: Royal Aircraft Establishment, Farnborough, Tech. note AERO.2677 (April 1960).

Bibliographical references: p. 18.