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Convective and radiative heat transfer during reentry and advanced techniques for their simulationThe use of shock tubes, ballistic ranges, and combinations thereof in simulation of convective and radiative heat loads has been described. The complementary nature and the highly independent techniques used in these facilities lend great strength to the research results where they agree. The shortcomings of these facilities are such that, if possible, both should be applied to important problems. When all-out performance is required, the combination of the two can clearly provide advantages. That these advantages are becoming more widely recognized is demonstrated by the construction of new faculties at Arnold Engineering Development Center and Boeing Company, Seattle, similar to those in service at Ames Research Center since the late 1950's.
Document ID
19650024005
Acquisition Source
Ames Research Center
Document Type
Other - Technical Report
Authors
Thomas N Canning
(Ames Research Center Mountain View, United States)
Date Acquired
August 2, 2013
Publication Date
July 1, 1965
Publication Information
Publication: The Role of Simulation in Space Technology: Part B
Publisher: National Aeronautics and Space Administration
Subject Category
Fluid Mechanics and Thermodynamics
Report/Patent Number
NASA-CR-64950
Meeting Information
Meeting: The Role of Simulation in Space and Technology
Location: Blacksburg, VA
Country: US
Start Date: August 17, 1964
End Date: August 21, 1964
Sponsors: National Science Foundation, National Aeronautics and Space Administration
Accession Number
65N33606
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Radiative Heat Transfer
Simulation
Reentry
Convective Heat Transfer
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