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A parametric analysis of radiative structure in aerobrake shock layersA broad-spectrum version of the NEQAIR code was modified to account for self-absorption and applied to AFE flowfields calculated by the LAURA code with a variety of kinetic models. The resulting radiative fluxes were obtained in a decoupled fashion from the flowfield solver along the vehicle's stagnation streamline. The radiative flux obtained was broken down by causative process to study the radiative structure of the AFE's flowfield for the various kinetic models. In addition, the radiative fluxes for several points on a typical AFE trajectory were analyzed to examine how the radiative structure changes as the vehicle completes its aeropass. Only two radiative processes dominated the stagnation radiative flux, and the flow field conditions near the wal were found to exert considerable influence over the radiative flux to the wall.
Document ID
19920064361
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Greendyke, Robert B.
(Vigyan, Inc. Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 92-2970
Accession Number
92A46985
Funding Number(s)
CONTRACT_GRANT: NAS1-19237
Distribution Limits
Public
Copyright
Other

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