The application of shock expansion theory to the flow outside regions influenced by the apex or tip on wings with supersonic edges
By: K. D. Thomson and L. M. Sheppard.
Contributors: Sheppard, L. M.; Aeronautical Research Laboratories (Australia)
Series: Aeronautical Research Laboratories. High Speed Aerodynamics Laboratory. Technical note -- no. HSA TN11
Publisher: High Speed Aerodynamics Laboratory
Published: 1954
Place of publication: Salisbury,  Australia
Notes: Bibliographical references: p. 2.