Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges
By: Y. C. Vigneron, J. V. Rakich and John C. Tannehill.
Contributors: Rakich, J. V.; Tannehill, John C.; AIAA
Publisher: AIAA
Published: 1978
Place of publication: New York
Number of pages: 19
Subjects: Delta wings; Leading edges; Supersonic flow; Viscous flow
Notes: Bibliographical references: p.14-15.

Source: AIAA 11th Fluid and Plasma Dynamics Conference, Seattle, Wash., July 10-12, 1978