Pressure distribution and momentum loss diagrams for the NACA profile 0 00 18 - 1.1 30 at high subsonic speed
By: translated by G.A. Awater.
Contributors: National Research Council of Canada. Division of Mechanical Engineering
Series: National Research Council of Canada. Technical translation -- no. TT-29
Publisher: National Research Council of Canada
Published: 1947
Place of publication: Ottawa
Notes: Bibliographical references: p. 2.

Translation of: Druckverteilungs und Impulsverlustschanbilder fur das Profil NACA 0 00 18 - 1.1 30 bei hohen Unterschallgeschwindigkeiten.