study of the flow around the leading edge of a highly-swept wing in a low-speed wind tunnel
By: by P. R. Ashil and C. J.Betts.
Contributors: Betts, C. J.; Defence Research Agency. Aerospace Division.
Series: Technical memorandum aerodynamics and propulsion -- 34
Publisher: Defence Research Agency
Published: 1993
Place of publication: Farnborough
Language: eng