Assessment of an All-Particle Hybrid Method for Hypersonic Rarefied Flow-Reference-Cited by-同舟云学术

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Assessment of an All-Particle Hybrid Method for Hypersonic Rarefied Flow

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Jun Eunji¹,Boyd Iain¹,Burt Jonathan²

Affiliation:

1. University of Michigan, Ann Arbor

2. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1203

Reference29 articles.

1. The Exploration of Mars; Historical Context and Current Results

2. 4AndersonJr,J.D.,Moderncompressibleflowwithhistoricalperspective,McGraw-Hill,NewYork,1990.

3. Mars Pathfinder rarefied aerodynamics - Computations and measurements

4. DSMC simulations of blunt body flows for Mars entries - Mars Pathfinder and Mars Microprobe capsules

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1. Aerodynamic Heating Analysis on Rocket Fairings Using CFD and DSMC;Journal of the Korean Society of Propulsion Engineers;2024-08-31

2. Comparative Study Between Cubic and Ellipsoidal Fokker–Planck Kinetic Models;AIAA Journal;2019-06

3. Assessment of the LD-DSMC hybrid method for hypersonic rarefied flow;Computers & Fluids;2018-04

4. Progress in particle-based multiscale and hybrid methods for flow applications;Microfluidics and Nanofluidics;2016-04

5. Validation and comparison between the low diffusion and DSMC method based on the 70° blunted cone test case;AIP Conference Proceedings;2016

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