Sensitivity of Hypersonic Dusty Flows to Physical Modeling of the Particle Phase-Reference-Cited by-同舟云学术

Sensitivity of Hypersonic Dusty Flows to Physical Modeling of the Particle Phase

Published:2021-05 Issue:3 Volume:58 Page:653-667
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Ching Eric¹,Barnhardt Michael²,Ihme Matthias¹

Affiliation:

1. Stanford University, Stanford, California 94305

2. NASA Ames Research Center, Mountain View, California 94035

Funder

Stanford University

National Aeronautics and Space Administration

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.A34810

Reference37 articles.

1. PapadopoulosP. E. “Computation of Heat Shield Erosion in a Dusty Martian Atmosphere,” Ph.D. Dissertation, Dept. of Aeronautics and Astronautics, Stanford Univ., Stanford, CA, 1994.

2. Reassessment of Effect of Dust Erosion on Heatshield of Mars Entry Vehicle

3. Numerical investigation of two-phase flow structure and heat transfer in a supersonic dusty gas flow over a blunt body

4. A two-way coupled Euler-Lagrange method for simulating multiphase flows with discontinuous Galerkin schemes on arbitrary curved elements

5. Effect of a Dispersed Admixture on the Flow Pattern and Heat Transfer in a Supersonic Dusty-Gas Flow Around a Cylinder

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