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: II. Uniform pitch and roll conditions
By: Hermann Behrbohm.
Contributors: Saab Aircraft Company
Series: Saab Aircraft Company. Technical note -- 21
Publisher: Saab Aircraft Company
Published: 1953
Place of publication: Linkoping, Sweden
Number of pages: 16
Notes: Bibliography: p. 16.