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Overview of NASA PTA propfan flight test programThe progress is covered of the NASA sponsored Propfan Test Assessment (PTA) flight test program. In PTA, a 9 ft. diameter propfan was installed on the left wing of a Gulfstream GII executive jet and is undergoing extensive flight testing to evaluate propfan structural integrity, near and far field noise, and cabin interior noise characteristics. This research testing includes variations in propeller tip speed and power loading, nacelle tilt angle, and aircraft Mach number and altitude. As a result, extensive parametric data will be obtained to verify and improve computer codes for predicting propfan aeroelastic, aerodynamic, and aeroacoustic characteristics. Over 600 measurements are being recorded for each of approx. 600 flight test conditions.
Document ID
19920013293
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Graber, Edwin J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1990
Publication Information
Publication: Aeropropulsion 1987
Subject Category
Aircraft Propulsion And Power
Accession Number
92N22536
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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