DTIC ADA042122: Development of a Three-Dimensional Combustor Flow Analysis. Volume II. Theoretical Studies.Report as inadecuate



 DTIC ADA042122: Development of a Three-Dimensional Combustor Flow Analysis. Volume II. Theoretical Studies.


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A three-dimensional computational procedure is presented for calculating the coupled flow and chemistry within rectangular or axisymmetric combustors with a discrete circumferential distribution of injection ports. The compressible time-averaged Navier-Stokes equations are solved with coupled pseudo-kinetic hydrocarbon chemistry including the effec

Author: Defense Technical Information Center

Source: https://archive.org/







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