What is it about?

In this paper, the rectangular exhaust nozzle test case from the 5th AIAA Propulsion Aerodynamics Workshop was studied for SetPoint 42. The conjugate-heat-transfer (CHT) and radiation models within the general-purpose CFD code, Ansys Fluent, have been used to assess the aerothermal interaction of the heated jet exhaust with a film-cooled plate downstream of a convergent nozzle exit.

Featured Image

Read the Original

This page is a summary of: Conjugate Heat Transfer Simulations of a Nozzle Flow over a Film-Cooled Plate, Journal of Thermophysics and Heat Transfer, December 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.t6595.
You can read the full text:

Read

Contributors

The following have contributed to this page