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Wind tunnel tests on a one-foot diameter SR-7L propfan modelWind tunnel tests have been conducted on a one-foot diameter model of the SR-7L propfan in the Langley 16-Foot and 4 x 7 Meter Wind Tunnels as part of the Propfan Test Assessment (PTA) Program. The model propfan was sized to be used on a 1/9-scale model of the PTA testbed aircraft. The model propeller was tested in isolation and wing-mounted on the aircraft configuration at various Mach numbers and blade pitch angles. Agreement between data obtained from these tests and data from Hamilton Standard validate that the 1/9-scale propeller accurately simulates the aerodynamics of the SR-7L propfan. Predictions from an analytical computer program are presented and show good agreement with the experimental data.
Document ID
19870058007
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Aljabri, Abdullah S.
(Lockheed-Georgia Co. Marietta, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1987
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 87-1892
Accession Number
87A45281
Funding Number(s)
CONTRACT_GRANT: NAS3-24339
Distribution Limits
Public
Copyright
Other

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