Add to ORKGTurbofan engine used for evaluating air jets as steady state inlet flow distortion devic
The F404-GE-400-powered F/A-18A High Alpha Research Vehicle (HARV) was used to examine the quality o...
Flow angle, static pressure, total temperature and total pressure were measured in the inlet duct up...
The P404-GF-400 Powered F/A-18A High Alpha Research Vehicle (HARV) was used to examine the impact of...
Performance and stall limits of afterburner-type turbofan engine with and without inlet flow distort...
A wind tunnel investigation was conducted to determine the amplitude and spatial distribution of ste...
The effects of the inlet pressure distortions, induced by five screen patterns, on the performance o...
Flow angle, static-pressure, and total-pressure distributions were measured in the passage ahead of ...
A review is presented of recent experimental results, analytical procedures and test techniques empl...
The measured effects of a circumferential distortion in inlet total pressure on the fan, low, and hi...
Military aircraft are often subjected to severe flight manoeuvres with high Angles of Attack (AOA) a...
Military aircraft are often subjected to severe flight maneuvers with high angles of attack and angl...
Several unique techniques and related devices are described which are in use at the Lewis Research C...
The effects of inlet-air-flow distortions on the performance of the J65-B-3 turbojet engine were det...
A program was conducted to reduce and analyze inlet and engine data obtained during testing of a TF3...
Performance data for high tip speed compressor rotor operated with radial and inlet airflow distorti...
The F404-GE-400-powered F/A-18A High Alpha Research Vehicle (HARV) was used to examine the quality o...
Flow angle, static pressure, total temperature and total pressure were measured in the inlet duct up...
The P404-GF-400 Powered F/A-18A High Alpha Research Vehicle (HARV) was used to examine the impact of...
Performance and stall limits of afterburner-type turbofan engine with and without inlet flow distort...
A wind tunnel investigation was conducted to determine the amplitude and spatial distribution of ste...
The effects of the inlet pressure distortions, induced by five screen patterns, on the performance o...
Flow angle, static-pressure, and total-pressure distributions were measured in the passage ahead of ...
A review is presented of recent experimental results, analytical procedures and test techniques empl...
The measured effects of a circumferential distortion in inlet total pressure on the fan, low, and hi...
Military aircraft are often subjected to severe flight manoeuvres with high Angles of Attack (AOA) a...
Military aircraft are often subjected to severe flight maneuvers with high angles of attack and angl...
Several unique techniques and related devices are described which are in use at the Lewis Research C...
The effects of inlet-air-flow distortions on the performance of the J65-B-3 turbojet engine were det...
A program was conducted to reduce and analyze inlet and engine data obtained during testing of a TF3...
Performance data for high tip speed compressor rotor operated with radial and inlet airflow distorti...
The F404-GE-400-powered F/A-18A High Alpha Research Vehicle (HARV) was used to examine the quality o...
Flow angle, static pressure, total temperature and total pressure were measured in the inlet duct up...
The P404-GF-400 Powered F/A-18A High Alpha Research Vehicle (HARV) was used to examine the impact of...