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Review of blunt body wake flows at hypersonic low density conditionsRecent results of experimental and computational studies concerning hypersonic flows about blunted cones including their near wake are reviewed. Attention is focused on conditions where rarefaction effects are present, particularly in the wake. The experiments have been performed for a common model configuration (70 deg spherically-blunted cone) in five hypersonic facilities that encompass a significant range of rarefaction and nonequilibrium effects. Computational studies using direct simulation Monte Carlo (DSMC) and Navier-Stokes solvers have been applied to selected experiments performed in each of the facilities. In addition, computations have been made for typical flight conditions in both Earth and Mars atmospheres, hence more energetic flows than produced in the ground-based tests. Also, comparisons of DSMC calculations and forebody measurements made for the Japanese Orbital Reentry Experiment (OREX) vehicle (a 50 deg spherically-blunted cone) are presented to bridge the spectrum of ground to flight conditions.
Document ID
19960029344
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Moss, J. N.
(NASA Langley Research Center Hampton, VA United States)
Price, J. M.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
June 20, 1996
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:111599
NASA-TM-111599
AIAA Paper 96-1803
Report Number: NAS 1.15:111599
Report Number: NASA-TM-111599
Report Number: AIAA Paper 96-1803
Meeting Information
Meeting: AIAA ThermophysicS Conference
Location: New Orleans, LA
Country: United States
Start Date: June 17, 1996
End Date: June 20, 1996
Accession Number
96N29796
Distribution Limits
Public
Copyright
Public Use Permitted.
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