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Low temperature simulation of subliming boundary layer flow in Jupiter atmosphereA low-temperature approximate simulation for the sublimation of a graphite heat shield under Jovian entry conditions is studied. A set of algebraic equations is derived to approximate the governing equation and boundary conditions, based on order-of-magnitude analysis. Characteristic quantities such as the wall temperature and the subliming velocity are predicted. Similarity parameters that are needed to simulate the most dominant phenomena of the Jovian entry flow are also given. An approximate simulation of the sublimation of the graphite heat shield is performed with an air-dry-ice model. The simulation with the air-dry-ice model may be carried out experimentally at a lower temperature of 3000 to 6000 K instead of the entry temperature of 14,000 K. The rate of graphite sublimation predicted by the present algebraic approximation agrees to the order of magnitude with extrapolated data. The limitations of the simulation method and its utility are discussed.
Document ID
19760054745
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chen, C. J.
(Iowa, University Iowa City, Iowa, United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 76-473
Meeting Information
Meeting: Thermophysics Conference
Location: San Diego, CA
Start Date: July 14, 1976
End Date: July 16, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
76A37711
Funding Number(s)
CONTRACT_GRANT: JPL-560015
Distribution Limits
Public
Copyright
Other

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