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Advanced general aviation propeller studyMethods for predicting the performance, noise, weight, and cost of propellers for advanced general aviation aircraft of the 1980 time period were developed and computerized. This basic program was refined to incorporate a method of including the blade shape parameter, integrated design lift coefficient. This method and a reverse thrust computational procedure were included in the computer program. The weight equation was refined and also incorporated in the computer program. A User's Manual which includes a complete listing of this computer program with detailed instructions on its use has been written.
Document ID
19720010354
Document Type
Contractor Report (CR)
Authors
Worobel, R. (Hamilton Standard Windsor Locks, CT, United States)
Mayo, M. G. (Hamilton Standard Windsor Locks, CT, United States)
Date Acquired
September 2, 2013
Publication Date
December 21, 1971
Subject Category
AIRCRAFT
Report/Patent Number
NASA-CR-114399
Funding Number(s)
CONTRACT_GRANT: NAS2-6477
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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NameType 19720010354.pdf STI