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Aerodynamic and propeller performance characteristics of a propfan-powered, semispan modelA semispan wing/body model with a powered propeller was tested to provide data on a total powerplant installation drag penalty of advanced propfan-powered aircraft. The test objectives were to determine the total power plant installation drag penalty on a representative propfan aircraft; to study the effect of configuration modifications on the installed powerplant drag; and to determine performance characteristics of an advanced design propeller which was mounted on a representative nacelle in the presence of a wing.
Document ID
19880004710
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Levin, Alan D.
(NASA Ames Research Center Moffett Field, CA, United States)
Smith, Ronald C.
(NASA Ames Research Center Moffett Field, CA, United States)
Wood, Richard D.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1985
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
A-85175
NAS 1.15:86705
NASA-TM-86705
Report Number: A-85175
Report Number: NAS 1.15:86705
Report Number: NASA-TM-86705
Accession Number
88N14092
Funding Number(s)
PROJECT: RTOP 535-03-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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