Computational Study of Vibrationally Relaxing Gas past Blunt Body in Hypersonic Flows-Reference-Cited by-同舟云学术

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Computational Study of Vibrationally Relaxing Gas past Blunt Body in Hypersonic Flows

Published:2000-01 Issue:1 Volume:14 Page:18-26
ISSN:0887-8722
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Josyula Eswar¹

Affiliation:

1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7913

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.6505

Reference18 articles.

1. Vibrationally Relaxing Flow of N past an Infinite Cylinder

2. Detailed simulation of nitrogen dissociation in stagnation regions

3. Nonequilibrium vibrational kinetics in the boundary layer of re-entering bodies

4. Prediction of Vibrational Relaxation in Hypersonic Expanding Flows Part 2: Results

5. Kinetic and gasdynamic processes in nonequilibrium molecular physics

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1. Slip boundary conditions for gas mixture flows with state-to-state vibrational-chemical kinetics;AIP Conference Proceedings;2024

2. First principles simulation of reacting hypersonic flow over a blunt wedge;Physics of Fluids;2023-08-01

3. Thermochemical Nonequilibrium Predictions for Nitrogen Flow over a Wedge;AIAA AVIATION 2022 Forum;2022-06-20

4. State-specific boundary conditions for nonequilibrium gas flows in slip regime;Physical Review E;2022-03-21

5. HyperCode: A framework for high-order accurate turbulent non-equilibrium hypersonic flow simulations;AIAA Scitech 2020 Forum;2020-01-05

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