The results presented are of a series of experimental tests in which a J85-13 turbojet engine was subjected to both distorted and undistorted inlet total pressure conditions. A distinctive feature of the data base obtained is that it includes compressor interstage information not previously recorded for a J85-13 engine. Each of the eight compressor stages was instrumented to obtain the characteristics of the individual stages for undistorted inlet conditions, and these data are documented in the report along with the undistorted compressor overall performance. Also included in the report is the overall performance of the compressor exposed to 14 different distorted-inlet conditions - 10 circumferential patterns and 4 radial patterns. The di...
An investigation to determine the steady-state and surge characteristics of the J57-P-1 two-spool tu...
Internal compressor instrumentation blockage effects on steady state J85-21 compressor performance a...
The results obtained in an inlet-engine compatibility test run in the 10x10 SWT of the NASA-Lewis Re...
The results presented are of a series of experimental tests in which a J85-13 turbojet engine was su...
The parallel compressor concept was studied using a compressor model based on the overall clean-inle...
The measured distribution of compressor interstage pressures and temperatures resulting from a 180 d...
The parallel compressor concept was studied using a compressor model based on the overall clean-inle...
Interstage data recorded on a J85-13 engine were used to analyze the internal flow of the compressor...
The measured effects of a circumferential distortion in inlet total pressure on the fan, low, and hi...
In order to effectively use a compressor face total-pressure distortion index as a measure of inlet-...
The primary objective of this research is to present results and methodologies used to study total p...
Effect of circumferential, radial, and combined pressure distortions on stall margin of J-85 engin
The effects of circumferential and radial temperature distortions and combined temperature and press...
The effects of the inlet pressure distortions, induced by five screen patterns, on the performance o...
The measured effects of inlet pressure distortion on the internal flow temperatures and pressures of...
An investigation to determine the steady-state and surge characteristics of the J57-P-1 two-spool tu...
Internal compressor instrumentation blockage effects on steady state J85-21 compressor performance a...
The results obtained in an inlet-engine compatibility test run in the 10x10 SWT of the NASA-Lewis Re...
The results presented are of a series of experimental tests in which a J85-13 turbojet engine was su...
The parallel compressor concept was studied using a compressor model based on the overall clean-inle...
The measured distribution of compressor interstage pressures and temperatures resulting from a 180 d...
The parallel compressor concept was studied using a compressor model based on the overall clean-inle...
Interstage data recorded on a J85-13 engine were used to analyze the internal flow of the compressor...
The measured effects of a circumferential distortion in inlet total pressure on the fan, low, and hi...
In order to effectively use a compressor face total-pressure distortion index as a measure of inlet-...
The primary objective of this research is to present results and methodologies used to study total p...
Effect of circumferential, radial, and combined pressure distortions on stall margin of J-85 engin
The effects of circumferential and radial temperature distortions and combined temperature and press...
The effects of the inlet pressure distortions, induced by five screen patterns, on the performance o...
The measured effects of inlet pressure distortion on the internal flow temperatures and pressures of...
An investigation to determine the steady-state and surge characteristics of the J57-P-1 two-spool tu...
Internal compressor instrumentation blockage effects on steady state J85-21 compressor performance a...
The results obtained in an inlet-engine compatibility test run in the 10x10 SWT of the NASA-Lewis Re...