A method of calculating the development of a supersonic jet exhausting into a subsonic free stream is presented. The method of characteristics is used with the conditions on the jet boundary modified by the change in static ...
An experimental investigation has been made to study the effect of casing wall boundary layers upon the rotating stall characteristics of an axial flow compressor in an isolated rotor row configuration. The boundary layer ...
Measurements have been made of the internal performance of a rectangular intake having variable geometry compression surfaces. The measurements have been made within a range of Mach numbers from 1.7 to 2.46 and at angles ...