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A prescribed wake rotor inflow and flow field prediction analysis, user's manual and technical approachA user's manual is provided which includes the technical approach for the Prescribed Wake Rotor Inflow and Flow Field Prediction Analysis. The analysis is used to provide the rotor wake induced velocities at the rotor blades for use in blade airloads and response analyses and to provide induced velocities at arbitrary field points such as at a tail surface. This analysis calculates the distribution of rotor wake induced velocities based on a prescribed wake model. Section operating conditions are prescribed from blade motion and controls determined by a separate blade response analysis. The analysis represents each blade by a segmented lifting line, and the rotor wake by discrete segmented trailing vortex filaments. Blade loading and circulation distributions are calculated based on blade element strip theory including the local induced velocity predicted by the numerical integration of the Biot-Savart Law applied to the vortex wake model.
Document ID
19820023420
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Egolf, T. A.
(United Technologies Research Center East Hartford, CT, United States)
Landgrebe, A. J.
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-165894
UTRC81-2
NAS 1.26:165894
Report Number: NASA-CR-165894
Report Number: UTRC81-2
Report Number: NAS 1.26:165894
Accession Number
82N31296
Funding Number(s)
CONTRACT_GRANT: NAS1-16058
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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