@inproceedings{52ba4725a2b14b638c0701595ef21564,
title = "Stage-by-stage dynamic compression system modeling for split core and bypass systems",
abstract = "A method for solving a set of equations for one-dimensional stage-by-stage dynamic compression system modeling was applied to a two-dimensional post-stall model. The model is suitable for capturing the flow during surge in split flow systems such as turbofans and, possibly, in centrifugal compressors. The modeling requires the solution of a modified form of the Euler equations in axisymmetric form. A robust solution method was facilitated by the use of a special form of upwind flux, flux difference splitting with source terms (FOSS), and implicit time integration. The modeling method was applied to the simulation of a split flow-",
author = "Lindau, {Jules W.} and O'Brien, {Walter F.}",
note = "Publisher Copyright: Copyright {\textcopyright} 1996 by ASME path fan system and results are presented.; ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1996 ; Conference date: 10-06-1996 Through 13-06-1996",
year = "1996",
doi = "10.1115/96-GT-279",
language = "English (US)",
series = "ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1996",
publisher = "American Society of Mechanical Engineers",
booktitle = "Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; General",
}