Heat flux predictions for hypersonic flows with an overset near body solver on an adaptive block-structured Cartesian off-body grid

Author:

McQuaid Joel A.ORCID,Brehm Christoph

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference48 articles.

1. CFD vision 2030 study: A path to revolutionary computational aerosciences;Slotnick,2014

2. Meakin RL, Wissink AM, Chan WM, Pandya SA, Sitaraman J. On Strand Grids for Complex Flows. In: 18th AIAA computational fluid dynamics conference. AIAA paper 2007-3834, Miami, Florida; 2007, p. 1–18. http://dx.doi.org/10.2514/6.2007-3834.

3. A sharp-interface immersed boundary method for high-speed compressible flows;Brahmachary,2020

4. Predictions of convective heat transfer using a cartesian grid solver for hypersonic flows;Sekhar,2013

5. Analysis of compressible viscous flow solvers with adaptive cartesian mesh;Arslanbekov,2011

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