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Turbulent Heat Transfer Experiments in Hypersonic Free Flight on Surfaces Representative of Woven TPS MaterialsMeasurements of turbulent rough-wall heat flux have been made in hypersonic flight in a ballistic range to characterized heat-flux augmentation on roughness patterns representative of woven thermal protection system materials.
Document ID
20205011354
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Michael C Wilder (Ames Research Center Mountain View, California, United States)
Dinesh K Prabhu (Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
December 9, 2020
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 2021 AIAA SciTech Forum
Location: Virtual
Country: US
Start Date: January 11, 2021
End Date: January 21, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 335803.04.22.21.10.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
heat transfer
roughness
hypersonic
ballistic range

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