Influence of Thermal Sensor Installation on Measuring Accuracy at Stagnation Points
Author:
Affiliation:
1. State Key Laboratory of High-Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, 100190 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
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
https://arc.aiaa.org/doi/pdf/10.2514/1.T4971
Reference15 articles.
1. Comparative study on aerodynamic heating under perfect and nonequilibrium hypersonic flows
2. An integral heat flux sensor with high spatial and temporal resolutions
3. Stagnation Heat Transfer and Through-Thickness Temperature Profile Calculation at Hypersonic Speeds
4. Stagnation-Point Flow and Heat Transfer of a Viscous, Compressible Fluid on a Cylinder
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