Measurement and simulation of hypersonic fluid-structural interaction on a cantilevered plate in a mach 6 flow

Gaetano M.D. Currao, Andrew J. Neely, David R. Buttsworth, Rishabh Choudhury

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

14 Citations (Scopus)

Abstract

The fluid-structural interaction of a cantilevered low-carbon steel plate oscillating and deforming plastically under the action of a hypersonic flow at Mach 5.8 was measured and simulated analytically and numerically. Displacement, flow field and surface pressure histories were measured during the fluid-structural interaction. High-speed schlieren video was used to simultaneously measure the displacement of the edge of the plate and the structure of the interacting compressible flow field including the position of shocks, expansions and the boundary layer. Fast response pressure-sensitive paint was used to map the history of pressure distribution on the surface of the plate. The plate was observed to deform plastically and this was accounted for in the FEM simulations. Experimental and numerical results showed partial agreement and suggestions for improving the experiment are discussed.

Original languageEnglish
Title of host publication15th Dynamics Specialists Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624103988
DOIs
Publication statusPublished - 2016
Event15th Dynamics Specialists Conference, 2016 - San Diego, United States
Duration: 2016 Jan 42016 Jan 8

Publication series

Name15th Dynamics Specialists Conference

Conference

Conference15th Dynamics Specialists Conference, 2016
Country/TerritoryUnited States
CitySan Diego
Period16-01-0416-01-08

All Science Journal Classification (ASJC) codes

  • Astronomy and Astrophysics
  • Aerospace Engineering

Fingerprint

Dive into the research topics of 'Measurement and simulation of hypersonic fluid-structural interaction on a cantilevered plate in a mach 6 flow'. Together they form a unique fingerprint.

Cite this