An analysis was made of the flow redistribution which occurs at the exit of an inlet due to the presence of a compressor. The flow redistribution includes a change in the axial velocity distortion, which is a function of the slope of the curve of compressor pressure coefficient versus flow coefficient at a particular corrected speed. (Author)
A Problem in Matching an Inlet and Engine Having Steady-State Circumferential Inlet Pressure Distortion
1970
16 pages
Report
Keine Angabe
Englisch
Effect of steady state inlet temperature distortion on the engine compressor flow
Tema Archiv | 1986
|Assessment of the Inlet/Engine Total Temperature Distortion Problem
SAE Technical Papers | 2017
A remark concerning engine-inlet distortion.
AIAA | 1968
|