Pressure distribution and momentum loss diagram for the NACA profile 0 00 12- 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. Division of Mechanical Engineering. Technical translation -- no. TT-27
Publisher: National Research Council of Canada
Published: 1947
Place of publication: Ottawa
Notes: Original German title: Druckverteilungs und Impulsverlustschaubilder fur das Profil NACA 0 00 12-1.1 30 bei Hohen Unterschallgeschwindigkeiten.