The effects of circumferential inlet temperature distortion on the flow characteristics between a distortion generator and a high bypass ratio turbofan engine and through its compression system were evaluated to support the effort to generate analytical models. The flow characteristics are defined by the inlet duct, the flow angles, and the total temperature, total pressure, and static pressure profiles in the inlet duct and through the fan and compressor. The effects of Reynolds number, rotor speed, and distortion extent are also considered
A wind tunnel investigation was conducted to determine the amplitude and spatial distribution of ste...
The effects of inlet-air-flow distortions on the performance of the J65-B-3 turbojet engine were det...
One of the possible origins of High Cycle Fatigue in a compressor blade is the rotating stall under ...
Flow angle, static pressure, total temperature and total pressure were measured in the inlet duct up...
Total-temperature, static-pressure and total-pressure distributions were measured in the inlet duct ...
Inlet temperature distortion effect on performance of turbofan engine compressor system
The effects of circumferential and radial temperature distortions and combined temperature and press...
The effects of steady-state and time-dependent fan inlet total temperature disturbances on the stabi...
An additional data base for improving and verifying a computer simulation developed by an engine man...
Flow angle, static-pressure, and total-pressure distributions were measured in the passage ahead of ...
The measured effects of inlet pressure distortion on the internal flow temperatures and pressures of...
A review is presented of recent experimental results, analytical procedures and test techniques empl...
The effects on stability of steady-state, 180 degree extent circumferential distortions of inlet tot...
The measured effects of a circumferential distortion in inlet total pressure on the fan, low, and hi...
An experimental investigation was conducted into the response of a small-turboshaft-engine compressi...
A wind tunnel investigation was conducted to determine the amplitude and spatial distribution of ste...
The effects of inlet-air-flow distortions on the performance of the J65-B-3 turbojet engine were det...
One of the possible origins of High Cycle Fatigue in a compressor blade is the rotating stall under ...
Flow angle, static pressure, total temperature and total pressure were measured in the inlet duct up...
Total-temperature, static-pressure and total-pressure distributions were measured in the inlet duct ...
Inlet temperature distortion effect on performance of turbofan engine compressor system
The effects of circumferential and radial temperature distortions and combined temperature and press...
The effects of steady-state and time-dependent fan inlet total temperature disturbances on the stabi...
An additional data base for improving and verifying a computer simulation developed by an engine man...
Flow angle, static-pressure, and total-pressure distributions were measured in the passage ahead of ...
The measured effects of inlet pressure distortion on the internal flow temperatures and pressures of...
A review is presented of recent experimental results, analytical procedures and test techniques empl...
The effects on stability of steady-state, 180 degree extent circumferential distortions of inlet tot...
The measured effects of a circumferential distortion in inlet total pressure on the fan, low, and hi...
An experimental investigation was conducted into the response of a small-turboshaft-engine compressi...
A wind tunnel investigation was conducted to determine the amplitude and spatial distribution of ste...
The effects of inlet-air-flow distortions on the performance of the J65-B-3 turbojet engine were det...
One of the possible origins of High Cycle Fatigue in a compressor blade is the rotating stall under ...
Add to ORKG