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ADPAC v1.0: User's ManualThe overall objective of this study was to evaluate the effects of turbulence models in a 3-D numerical analysis on the wake prediction capability. The current version of the computer code resulting from this study is referred to as ADPAC v7 (Advanced Ducted Propfan Analysis Codes -Version 7). This report is intended to serve as a computer program user's manual for the ADPAC code used and modified under Task 15 of NASA Contract NAS3-27394. The ADPAC program is based on a flexible multiple-block and discretization scheme permitting coupled 2-D/3-D mesh block solutions with application to a wide variety of geometries. Aerodynamic calculations are based on a four-stage Runge-Kutta time-marching finite volume solution technique with added numerical dissipation. Steady flow predictions are accelerated by a multigrid procedure. Turbulence models now available in the ADPAC code are: a simple mixing-length model, the algebraic Baldwin-Lomax model with user defined coefficients, the one-equation Spalart-Allmaras model, and a two-equation k-R model. The consolidated ADPAC code is capable of executing in either a serial or parallel computing mode from a single source code.
Document ID
19990028620
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hall, Edward J.
(Allison Engine Co. Indianapolis, IN United States)
Heidegger, Nathan J.
(Allison Engine Co. Indianapolis, IN United States)
Delaney, Robert A.
(Allison Engine Co. Indianapolis, IN United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1999
Subject Category
Aerodynamics
Report/Patent Number
NASA/CR-1999-206600
E-11089
NAS 1.26:206600
Report Number: NASA/CR-1999-206600
Report Number: E-11089
Report Number: NAS 1.26:206600
Funding Number(s)
PROJECT: RTOP 538-03-11
CONTRACT_GRANT: NAS3-27394
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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