An innovative inlet total pressure distortion measurement rake has been designed and developed for the F/A-18 A/B/C/D aircraft inlet. The design was conceived by NASA and General Electric Aircraft Engines personnel. This rake has been flight qualified and flown in the F/A-18 High Alpha Research Vehicle at NASA Dryden Flight Research Center, Edwards, California. The eight-legged, one-piece, wagon wheel design of the rake was developed at a reduced cost and offered reduced installation time compared to traditional designs. The rake features 40 dual-measurement ports for low- and high-frequency pressure measurements with the high-frequency transducer mounted at the port. This high-frequency transducer offers direct absolute pressure measuremen...
Future aircraft turbine engines, both commercial and military, will have to be able to successfully ...
A submerged inlet investigation, using flow control in the form of discrete blowing, examined proxim...
An investigation was conducted to evaluate and improve the quality of the airflow to be supplied to ...
An innovative inlet total-pressure distortion measurement rake has been designed and developed for t...
The effects of high-angle-of-attack flight on aircraft inlet aerodynamic characteristics were invest...
The Propulsion Flight Test Fixture at the NASA Dryden Flight Research Center is a unique test platfo...
The Rake Airflow Gage Experiment involves a flow-field survey rake that was flown on the Propulsion ...
The performance and distortion levels of the right inlet of the F/A-18A High Alpha Research Vehicle ...
A compressor face rake with an internal valve arrangement to permit nulling was designed, constructe...
Rake mounting design reduces aerodynamic-surface discontinuities to a minimum when installed in boun...
The F404-GE-400-powered F/A-18A High Alpha Research Vehicle (HARV) was used to examine the quality o...
An experimental measurement system was developed and implemented by the NASA Glenn Research Center i...
A 15 percent scale lightweight fighter type inlet forebody was tested in the Ames 14 foot transonic ...
The NASA Glenn Research Centers DGEN Aeropropulsion Research Turbofan (DART) is based on the Price I...
The results of a low-speed wind tunnel test of a 0.3 scale model 727 airplane side inlet for JT8D-10...
Future aircraft turbine engines, both commercial and military, will have to be able to successfully ...
A submerged inlet investigation, using flow control in the form of discrete blowing, examined proxim...
An investigation was conducted to evaluate and improve the quality of the airflow to be supplied to ...
An innovative inlet total-pressure distortion measurement rake has been designed and developed for t...
The effects of high-angle-of-attack flight on aircraft inlet aerodynamic characteristics were invest...
The Propulsion Flight Test Fixture at the NASA Dryden Flight Research Center is a unique test platfo...
The Rake Airflow Gage Experiment involves a flow-field survey rake that was flown on the Propulsion ...
The performance and distortion levels of the right inlet of the F/A-18A High Alpha Research Vehicle ...
A compressor face rake with an internal valve arrangement to permit nulling was designed, constructe...
Rake mounting design reduces aerodynamic-surface discontinuities to a minimum when installed in boun...
The F404-GE-400-powered F/A-18A High Alpha Research Vehicle (HARV) was used to examine the quality o...
An experimental measurement system was developed and implemented by the NASA Glenn Research Center i...
A 15 percent scale lightweight fighter type inlet forebody was tested in the Ames 14 foot transonic ...
The NASA Glenn Research Centers DGEN Aeropropulsion Research Turbofan (DART) is based on the Price I...
The results of a low-speed wind tunnel test of a 0.3 scale model 727 airplane side inlet for JT8D-10...
Future aircraft turbine engines, both commercial and military, will have to be able to successfully ...
A submerged inlet investigation, using flow control in the form of discrete blowing, examined proxim...
An investigation was conducted to evaluate and improve the quality of the airflow to be supplied to ...