26th Aerospace Sciences Meeting 1988
DOI: 10.2514/6.1988-274
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The application of Euler and Navier-Stokes methodology to 2-D and 3-D nozzle-afterbody flowfields

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“…More accurate predictions of far-field pressure distribution, local Mach number distribution, and separation point were achieved by coupling the viscous and inviscid flow computations. Bergman and Treiber [10] modelled the inviscid and three-dimensional flow surrounding the nozzle using Euler's equation and found that the viscosity and three-dimensional effects play an important role in the properties of surrounding flow field. Numerical study on an overexpanded subscale nozzle (J-2S) was conducted by Chen et al [11].…”
Section: Introductionmentioning
confidence: 99%
“…More accurate predictions of far-field pressure distribution, local Mach number distribution, and separation point were achieved by coupling the viscous and inviscid flow computations. Bergman and Treiber [10] modelled the inviscid and three-dimensional flow surrounding the nozzle using Euler's equation and found that the viscosity and three-dimensional effects play an important role in the properties of surrounding flow field. Numerical study on an overexpanded subscale nozzle (J-2S) was conducted by Chen et al [11].…”
Section: Introductionmentioning
confidence: 99%