Experimental determination of pressure distributions and transition lines of plane delta wings at low speeds and zero yaw
By: Kazimierz Orlik-Ruckemann.
Contributors: Royal Institute of Technology (Sweden). Division of Aeronautics
Series: Royal Institute of Technology. Division of Aeronautics. Technical note -- 3
Publisher: Royal Institute of Technology, Division of Aeronautics
Published: 1948
Place of publication: Stockholm
Number of pages: 47
Notes: Bibliographical references: p. 8.