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Fluidic Injection Scenarios for Shock Pattern Manipulation in Exhausts

Accepted version
Peer-reviewed

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Abstract

By numerically screening internal fluidic injection scenarios for the manipulation of the double diamond shock pattern in convergent–divergent nozzle exhausts, the individual importance of design parameters is demonstrated. It is found that the evolving shock pattern is sensitive to the injection location, whereas the persistence of the induced counterrotating vortex pairs is primarily governed by the injection pressure. Injection close to the nozzle exit generates secondary vortical structures, amplifying the fluctuations in the nozzle vicinity.

Description

Journal Title

AIAA Journal

Conference Name

Journal ISSN

0001-1452
1533-385X

Volume Title

56

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

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