Approximate theoretical pressure distribution due to lift and uniform pitch and roll for double-delta wings with subsonic leading edges at supersonic speeds
By: Volrath Holmboe.
Contributors: Saab Aircraft Company
Series: Saab Aircraft Company. Technical note -- 28
Publisher: Saab Aircraft Company
Published: 1954
Place of publication: Linkoping, Sweden
Number of pages: 21
Notes: Bibliography: p. 10.