Measurements of Surface Heating from Hypersonic Boundary Layer Transition by Simultaneous Temperature-Sensitive Paint and Infrared Thermography-Reference-Cited by-同舟云学术

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Measurements of Surface Heating from Hypersonic Boundary Layer Transition by Simultaneous Temperature-Sensitive Paint and Infrared Thermography

Published:2024-01-04 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2024 Forum
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Author:

Smith Cary D.¹,Siddiqui Farhan¹,Ledbetter Shelby¹,Gragston Mark¹,Shine Jack S.²,Ibanez Oscar²,McGruder Donovan²,Bowersox Rodney D.²

Affiliation:

1. The University of Tennessee Space Institute

2. Texas A&M University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2024-0667

Reference17 articles.

1. Bontrager, P. J. "Development of Thermocouple Type Total Temperature Probes in the Hypersonic Flow Regime," Ph.D. thesis,University of Tennessee, 1968.

2. Verification of quantitative infrared thermography heat-flux measurements

3. Fast-response temperature-sensitive-paint measurements on a hypersonic transition cone

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