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AFFDL-TR-79-3078 ^öj^f%jw NUMERICAL SOLUTION OF A SUPERSONIC NOZZLE AFTERBODY FLOW WITH JET EXHAUSTAmeer G. Mikhail2012

Performance of a Vectorized Three-Dimensional Navier-Stokes Code on the CRAY-] Computer,J. S. Shang, P. G. Buning, W. L. Hankey, Wirth, M. rAIAA Journal,1980

Evaluation of Turbulence Models for Rocket and Aircraft Plume Flowfield Predictions,H. S. Pergament, S. M. Dash, A. K. VarmaARAP Report No1979

Numerical Simulation of MultiStream Nozzle Flows," AIAA Paper 79-1549K. M. Peery, C. K. ForesterAIAA 12th Fluid and Plasma Dynamics Confere!.ce,1979

Overlaid Viscous/Inviscid Model for the Prediction of Near Field Jet Entrainment,S. M. Dash, R. G. Wilmouth, H. S. PergamentAIAA Journal,1979

Prediction of Nearfield Jet Entrainment by an Interactive Mixing/Afterburning Model," AIAA Paper 78-1189H. S. Pergament, S. M. Dash, R. G. Wilmoth1978

Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows," AIAA Paper 78-527B. S. Baldwin, H. Lomax1978

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