Direct simulation calculations of the rarefied flow past a forward-facing step
Author:
Affiliation:
1. University of Melbourne, Parkville, Australia
2. Imperial College, London, England
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.7310
Reference10 articles.
1. Direct Simulation and the Boltzmann Equation
2. Aerodynamic properties of some simple bodies in the hypersonic transition regime.
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2. DSMC simulation of rarefied gas flow over a forward-facing step: Effect of expansion ratio;ADVANCED TRENDS IN MECHANICAL AND AEROSPACE ENGINEERING: ATMA-2019;2021
3. Effect of Mach Number on the Rarefied Gas Flow Over a Forward-Facing Step;Lecture Notes in Mechanical Engineering;2021
4. Changing the regime of supersonic flow past a rectangular step using gas-permeable inserts;Technical Physics Letters;2015-09
5. Computational analysis of the flow field structure of a non-reacting hypersonic flow over forward-facing steps;Journal of Fluid Mechanics;2014-12-18
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