The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack
By: Torsten Berglind, Georg Drougge and Peter Eliasson.
Contributors: Drougge, Georg.; Eliasson, Peter.; The Aeronautical Research Institute of Sweden
Series: FFA meddelande -- 141; FFA report -- 141
Publisher: Aeronautical Research Institute of Sweden
Published: 1988
Place of publication: Stockholm
Number of pages: 12
Subjects: Delta wings; Supersonic drag
Notes: Bibliographical references: p.11-12.