A semi-numerical method for the determination of the disturbance velocity potential and the pressure distribution of double-delta wings with subsonic leading edges in supersonic flow: I. Symmetrical flow conditions
By: Hermann Behrbohm.
Contributors: Saab Aircraft Company
Series: Saab Aircraft Company. Technical note -- 20
Publisher: Saab Aircraft Company
Published: 1953
Place of publication: Linkoping, Sweden
Number of pages: 18
Notes: Bibliography: p. 17-18.