Month in the Patent Office

Abstract

A probe 1 having a static pressure detecting point 1a is mounted on a transonic aircraft fin 4 in a rearwardly directed position in order that the point 1a is situated in an undisturbed zone aft of the rearmost pressure wave 03 and substantially downstream of the turbulent wake zone of the aircraft over a range of speeds including 0·85–1·1 Mach.

Citation

(1958), "Month in the Patent Office", Aircraft Engineering and Aerospace Technology, Vol. 30 No. 12, pp. 384-384. https://doi.org/10.1108/eb033060