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Development of a rotor wake-vortex model, volume 1Certain empirical rotor wake and turbulence relationships were developed using existing low speed rotor wave data. A tip vortex model was developed by replacing the annulus wall with a row of image vortices. An axisymmetric turbulence spectrum model, developed in the context of rotor inflow turbulence, was adapted to predicting the turbulence spectrum of the stator gust upwash.
Document ID
19850018357
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Majjigi, R. K.
(General Electric Co. Cincinnati, OH, United States)
Gliebe, P. R.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:174849
NASA-CR-174849
Report Number: NAS 1.26:174849
Report Number: NASA-CR-174849
Accession Number
85N26668
Funding Number(s)
CONTRACT_GRANT: NAS3-23681
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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