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Turbofan forced mixer lobe flow modeling. 2: Three-dimensional inviscid mixer analysis (FLOMIX)A three-dimensional potential analysis (FLOMIX) was formulated and applied to the inviscid flow over a turbofan foced mixer. The method uses a small disturbance formulation to analytically uncouple the circumferential flow from the radial and axial flow problem, thereby reducing the analysis to the solution of a series of axisymmetric problems. These equations are discretized using a flux volume formulation along a Cartesian grid. The method extends earlier applications of the Cartesian method to complex cambered geometries. The effects of power addition are also included within the potential formulation. Good agreement is obtained with an alternate small disturbance analysis for a high penetration symmetric mixer in a planar duct. In addition, calculations showing pressure distributions and induced secondary vorticity fields are presented for practical trubofan mixer configurations, and where possible, comparison was made with available experimental data. A detailed description of the required data input and coordinate definition is presented along with a sample data set for a practical forced mixer configuration. A brief description of the program structure and subroutines is also provided.
Document ID
19890004851
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Barber, T.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1988
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:4147-PT-2
NASA-CR-4147-PT-2
E-4084
Report Number: NAS 1.26:4147-PT-2
Report Number: NASA-CR-4147-PT-2
Report Number: E-4084
Accession Number
89N14222
Funding Number(s)
PROJECT: RTOP 505-62-21
CONTRACT_GRANT: NAS3-23039
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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