Nanosecond CARS Measurements of Temperature and Relative CO Concentration in the Boundary Layer of a Graphite Ablator in an Inductively Coupled Plasma Torch
Author:
Affiliation:
1. The University of Texas at Austin
2. Sandia National Laboratories
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-0446
Reference31 articles.
1. Radiative heating predictions for Huygens entry
2. Chemical-Kinetic Parameters of Hyperbolic Earth Entry
3. Viscous Shock-Layer Simulation of Airflow past Ablating Blunt Body with Carbon Surface
4. Finite-Rate Surface Chemistry Model, II: Coupling to Viscous Navier-Stokes Code
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. HyperMATE: A Novel Aerothermal Testing Facility at the University of Tennessee;Journal of Thermal Science and Engineering Applications;2024-08-29
2. Laser-Induced Fluorescence for Temperature and Density of CN and CO in the Boundary Layer of Graphite Ablation in an Inductively-Coupled Plasma Torch Plume;AIAA SCITECH 2024 Forum;2024-01-04
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