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A comparison between implicit and hybrid methods for the calculation of steady and unsteady inlet flowsNumerical simulation of steady and unsteady transonic diffuser flows using two different computer codes are discussed and compared with experimental data. The codes solve the Reynolds-averaged, compressible, Navier-Stokes equations using various turbulence models. One of the codes has been applied extensively to diffuser flows and uses the hybrid method of MacCormack. This code is relatively inefficient numerically. The second code, which was developed more recently, is fully implicit and is relatively efficient numerically. Simulations of steady flows using the implicit code are shown to be in good agreement with simulations using the hybrid code. Both simulations are in good agreement with experimental results. Simulations of unsteady flows using the two codes are in good qualitative agreement with each other, although the quantitative agreement is not as good as in the steady flow cases. The implicit code is shown to be eight times faster than the hybrid code for unsteady flow calculations and up to 32 times faster for steady flow calculations. Results of calculations using alternative turbulence models are also discussed.
Document ID
19850059266
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Coakley, T. J.
(NASA Ames Research Center Moffett Field, CA, United States)
Hsieh, T.
(U.S. Navy, Naval Surface Weapons Center White Oak, MD, United States)
Date Acquired
August 12, 2013
Publication Date
July 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 85-1125
Accession Number
85A41417
Distribution Limits
Public
Copyright
Other

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