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Results of the integration of a transonic full-potential analysis program with a free-wake lifting-line program for hovering rotorsThe hovering performance predictions of the TFAR1 and OPLIN codes and the experimental data are discussed. The TFAR1 program solves the full-potential equation in a rotor-fixed coordinate system by use of the line relaxation method. The OPLIN program calculates the positions of wake vortices and rotor performance using the influence-coefficient-and-lifing-line method. The two programs are combined by adding the induced velocities from the OPLIN code to the near flow-field of the rotor from the TFAR1 code. Results show that the TFAR1 program converges better with the downwash-coupling method than the twist correction method to include the wake downwash.
Document ID
19870013198
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Chung, Song-Young
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1987
Subject Category
Aerodynamics
Report/Patent Number
A-87193
NASA-TM-89494
NAS 1.15:89494
Report Number: A-87193
Report Number: NASA-TM-89494
Report Number: NAS 1.15:89494
Accession Number
87N22631
Funding Number(s)
PROJECT: RTOP 505-61-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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