method of upwash-cancellation in linearized supersonic wing theory as applied to the double-delta wing with subsonic leading edges. II. Velocity potential and pressure distribution at symmetrical flow conditions
By: Hermann Behrbohm.
Contributors: Saab Aircraft Company
Series: Saab Aircraft Company -- Technical note ; 19
Publisher: Saab Aircraft Company
Published: 1953
Place of publication: Linkoping, Sweden
Number of pages: 25