Numerical study of shock-turbulent boundary layer interactions with incipient and complete separation. (1st January 2011)

• Record Type: Journal Article
• Authors: Agostini, Lionel; Dupont, Pierre; Larchevêque, Lionel; Dussauge, Jean Paul
• Is Part Of: International journal of engineering systems modelling and simulation. Volume 3:Number 1/2(2011)
• Page Start: 46
• Page End: 52
• Publication Date: 2011-01-01
• Subjects: shock boundary layer interactions -- unsteadiness in separated flows -- supersonic turbulent boundary layers; Engineering systems -- Computer simulation -- Periodicals; Engineering systems -- Mathematical models -- Periodicals; 620.0042
• DOI: 10.1504/IJESMS.2011.038749
• Languages: English
• ISSNs: 1755-9758

Abstract

This paper aims at describing the main features of a separated boundary layer in shock reflection at a Mach number of 2.3. The data used for this analysis were taken from large eddy simulations of the interactions for three-shock intensities, resulting in flow cases from incipient to fully separated. Computational results were validated versus experimental data. The main space-time properties of the reflected shock motion are described together with their link with the other flow regions. The analysis of the correlations between the shock motion and the unsteady pressure field provides information about the origins of shock unsteadiness.