Development of stability analysis tools for high speed compressible flows

Rutvij R. Bhagwat, Pramod K. Subbareddy

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

We present some recent work related to the development of stability analysis tools for high speed compressible flows. High speed flows are often dominated by shocks, and exhibit a host of other interacting flow features such as boundary layers and acoustic waves. Techniques such as global stability analysis and resolvent analysis are useful for the analysis of these flows. Some validation results for simple configurations such as a compressible mixing layer, compressible boundary layer, incompressible flow over a cylinder, and incompressible channel flow are presented. Results for a hypersonic flow over a wedge have been discussed along with potential for future work.

Original languageEnglish (US)
Title of host publication2018 Fluid Dynamics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105531
DOIs
StatePublished - 2018
Externally publishedYes
Event48th AIAA Fluid Dynamics Conference, 2018 - Atlanta, United States
Duration: Jun 25 2018Jun 29 2018

Publication series

Name2018 Fluid Dynamics Conference

Other

Other48th AIAA Fluid Dynamics Conference, 2018
CountryUnited States
CityAtlanta
Period6/25/186/29/18

Fingerprint Dive into the research topics of 'Development of stability analysis tools for high speed compressible flows'. Together they form a unique fingerprint.

Cite this