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Three Dimensional Compressible Turbulent Flow Computations For A Diffusing S Duct With Without Vortex Generators

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Three Dimensional Compressible Turbulent Flow Computations For A Diffusing S Duct With Without Vortex Generators

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Author : Soo-Yong Cho
language : en
Publisher:
Release Date : 1994

Three Dimensional Compressible Turbulent Flow Computations For A Diffusing S Duct With Without Vortex Generators written by Soo-Yong Cho and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with categories.

Three Dimensional Compressible Turbulent Computations For A Diffusing S Duct

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Author :
language : en
Publisher:
Release Date : 1992

Three Dimensional Compressible Turbulent Computations For A Diffusing S Duct written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Air ducts categories.

Three Dimensional Compressible Turbulent Computations For A Diffusing S Duct

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Author : C. F. Smith
language : en
Publisher:
Release Date : 1992

Three Dimensional Compressible Turbulent Computations For A Diffusing S Duct written by C. F. Smith and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with categories.

Three Dimensional Compressible Turbulent Computations For A Diffusing S Duct

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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-08-20

Three Dimensional Compressible Turbulent Computations For A Diffusing S Duct written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-08-20 with categories.

The purpose of the present study was to evaluate the capability of the computational fluid dynamics computer program PARC3D to model flow in a typical diffusing subsonic S-duct, with strong secondary flows. This evaluation is needed to provide confidence in the analysis of aircraft inlets, which have similar geometries. The performance predictions include total pressure profiles, static pressures, velocity profiles, boundary layer data, and skin friction data. Flow in the S-duct is subsonic, and the boundary layers are assumed to be turbulent. The results for both H and O grid solutions, are compared with existing test data. Smith, C. F. and Bruns, J. E. and Harloff, G. J. and Debonis, J. R. Unspecified Center NAS3-25266; RTOP 533-02-30...

Three Dimensional Compressible Turbulent Computations For A Nondiffusing S Duct

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Author :
language : en
Publisher:
Release Date : 1992

Three Dimensional Compressible Turbulent Computations For A Nondiffusing S Duct written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Air ducts categories.

Three Dimensional Compressible Turbulent Computations For A Nondiffusing S Duct

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Author : G. J. Harloff
language : en
Publisher:
Release Date : 1992

Three Dimensional Compressible Turbulent Computations For A Nondiffusing S Duct written by G. J. Harloff and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with categories.

Three Dimensional Compressible Turbulent Computations For A Nondiffusing S Duct

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Author : National Aeronautics and Space Adm Nasa
language : en
Publisher: Independently Published
Release Date : 2018-10-15

Three Dimensional Compressible Turbulent Computations For A Nondiffusing S Duct written by National Aeronautics and Space Adm Nasa and has been published by Independently Published this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-10-15 with Science categories.

The PARC3D code was used to compute the compressible turbulent flow within a three dimensional, nondiffusing S-duct. A frame of reference is provided for future computational fluid dynamics studies of internal flows with strong secondary flows and provides an understanding of the performance characteristics of a typical S-duct with attached flow. The predicted results, obtained with both H- and O-grids, are compared with the experimental wall pressure, static and total pressure fields, and velocity vectors. Additionally, computed boundary layer thickness, velocity profiles in wall coordinates, and skin friction values are presented. Harloff, G. J. and Debonis, J. R. and Smith, C. F. and Bruns, J. E. Unspecified Center NAS3-25266; RTOP 533-02-30