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Research on the statically thrusting propellerMethods for calculating the induced flow at propeller blades were analyzed by treating the wake formation as an initial problem in time. An unsteady vortex lattice technique was applied to the wake formation and the vortex core size was studied.
Document ID
19780017149
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Eisenhuth, J. J. (Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-157214
Report Number: NASA-CR-157214
Accession Number
78N25092
Funding Number(s)
CONTRACT_GRANT: NGL-39-009-172
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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