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Low-to-high altitude predictions of three-dimensional ablative reentry flowfieldsA new coupled-chemistry PNS scheme has been developed to study 3D hypersonic reentry flows over sphere cones at small angles of attack. A new quasi-steady ablation model for Teflon was used to predict ablative reentry flow fields under laminar, transitional, and turbulent conditions. This solution scheme uses a new two-step solution scheme for solving the species conservation equations under low-altitude conditions. As an example, the scheme is used to study hypersonic flow over a 6-deg sphere-cone configuration at 50 and 125 kft conditions under zero and nonzero angle of attack conditions.
Document ID
19920043603
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bhutta, Bilal A.
(NASA Lewis Research Center Cleveland, OH, United States)
Lewis, Clark H.
(VRA, Inc. Blacksburg, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 92-0366
Report Number: AIAA PAPER 92-0366
Accession Number
92A26227
Funding Number(s)
CONTRACT_GRANT: NAS3-25450
Distribution Limits
Public
Copyright
Other

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