Direct simulation calculations of the rarefied flow past a forward-facing step

AIAA Journal ◽  
1977 ◽  
Vol 15 (1) ◽  
pp. 124-126 ◽  
Author(s):  
D. I. Pullin ◽  
J. K. Harvey
AIAA Journal ◽  
2016 ◽  
Vol 54 (5) ◽  
pp. 1670-1681 ◽  
Author(s):  
Benzi John ◽  
Xiao-Jun Gu ◽  
Robert W. Barber ◽  
David R. Emerson

1996 ◽  
Vol 312 ◽  
pp. 149-172 ◽  
Author(s):  
Michael A. Gallis ◽  
John K. Harvey

In this paper the phenomenon of chemical reactivity in hypersonic rarefied flows is examined. A new model is developed to describe the reactions and post-collision energy exchange processes that take place under conditions of molecular non-equilibrium. The new scheme, which is applied within the framework of the direct simulation Monte Carlo (DSMC) method, draws its inspiration from the principles of maximum entropy which were developed by Levine & Bernstein. Sample hypersonic flow fields, typical of spacecraft re-entry conditions in which reactions play an important role, are presented and compared with results from experiments and other DSMC calculations. The latter use traditional methods for the modelling of chemical reactions and energy exchange. The differences are discussed and evaluated.


2021 ◽  
Vol 33 (9) ◽  
pp. 097105
Author(s):  
He Zhang ◽  
Fanli Shan ◽  
Hong Fang ◽  
Xing Zhang ◽  
Jun Zhang ◽  
...  

Author(s):  
X. J. Gu ◽  
D. R. Emerson

Abstract A high-order moment method is employed to study the effect of the wall temperature on gas flow past a stationary circular cylinder in terms of the size of the vortices behind the cylinder and the drag coefficient. When the wall temperature is lower than the free stream temperature, flow separation occurs at a lower Reynolds number and the vortex length is elongated with a corresponding reduction in the drag coefficient. Conversely, increasing the wall temperature above the free stream temperature delays the onset of flow separation and increases the drag coefficient.


Sign in / Sign up

Export Citation Format

Share Document