## Viscous-inviscid Aerodynamic Analysis of Two-dimensional Thrust Augmentors |

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analysis analytically approximation arbitrary shape assumed assumption augmentation ratio augmentor performance axis Borda mouthpiece solution boundary conditions boundary layer calculation Components of inviscid conformal mapping conservation of mass diffuser angle diffuser area ratio diffuser length end of region equation of conservation exhaust plume exit pressure EXPERIMENTS REF finite differences flat plates flow field induced Flow induced free jet global Hence ical incompressible infinitely far downstream infinity inlet plane inner flow inner solution integral in 2.52 integral method inviscid flow field Neglecting outer field outer flow overall length parallel walls perturbation approach perturbed Borda component physical plane primary jet entrainment problem resulting outer results are compared Reynolds stress right hand side Schwartz-Christofeln theorem secondary flow shown in figure sink solved stream function substituting theory thrust augmentation transformation 2.6 transformed plane turbulent jet upper half velocity distribution velocity field velocity profile virtual origin viscous solution viscous-inviscid interaction