NASA Technical Reports Server (NTRS) 19820008209: A Computer Code for Swirling Turbulent Axisymmetric Recirculating Flows in Practical Isothermal Combustor GeometriesReport as inadecuate



 NASA Technical Reports Server (NTRS) 19820008209: A Computer Code for Swirling Turbulent Axisymmetric Recirculating Flows in Practical Isothermal Combustor Geometries


NASA Technical Reports Server (NTRS) 19820008209: A Computer Code for Swirling Turbulent Axisymmetric Recirculating Flows in Practical Isothermal Combustor Geometries - Download this document for free, or read online. Document in PDF available to download.

Download or read this book online for free in PDF: NASA Technical Reports Server (NTRS) 19820008209: A Computer Code for Swirling Turbulent Axisymmetric Recirculating Flows in Practical Isothermal Combustor Geometries
A primitive pressure-velocity variable finite difference computer code was developed to predict swirling recirculating inert turbulent flows in axisymmetric combustors in general, and for application to a specific idealized combustion chamber with sudden or gradual expansion. The technique involves a staggered grid system for axial and radial veloc

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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