Experimental determination of pressure distributions and transition lines of plane delta wings at low speeds and zero yaw
By: K. Orlik-Ruckemann
Contributors: Kungl. Tekniska högskolan
Series: Kungl. Tekniska högskolan aero technical note -- 3
Publisher: Royal Institute of Technology
Published: 1948
Place of publication: Stockholm
Language: eng
Number of pages: 47
Notes: Cover title.