NUMERICAL SIMULATION OF SHOCK/BOUNDARY-LAYER INTERACTION USING A TWO-EQUATION TURBULENCE MODEL.

G. R. Peters, R. K. Agarwal, J. E. Deese

Research output: Contribution to journalConference articlepeer-review

Abstract

At transonic speeds, shock waves appear in flowfields about aircraft wings, in turbomachinery blade passages, and in air-breathing-engine inlets and diffusers. The interactions of these shock waves with turbulent boundary layers on the solid surfaces results in complex flow phenomena. In this paper, we study the shock/boundary interaction flows by numerically solving the mass-averaged compressible thin-layer Navier-Stokes equations in conjunction with a zero-equation Baldwin-Lomax and a two-equation turbulence model.

Original languageEnglish
Pages (from-to)485
Number of pages1
JournalDevelopments in Mechanics
Volume13
StatePublished - 1985

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