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Performance estimation for highly loaded six and ten blade propellers combined with an advanced technology turboshaft enginePerformance estimations, weights, and scaling laws for the six blade and ten blade highly loaded propellers combined with an advanced turboshaft engine are presented. These data are useful for aircraft mission studies using the turboprop system. Comparisons are made between the performance of post 1980 technology turboprop propulsion systems and the performance of both a current technology turbofan and a post 1990 technology turbofan.
Document ID
19800019852
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Morris, S. J., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-81840
Report Number: NASA-TM-81840
Accession Number
80N28353
Funding Number(s)
PROJECT: RTOP 533-01-43-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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