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Complex three-dimensional internal flows in the ASRM and RSRM aft end segmentsResults from computational fluid dynamic analyses for complex three dimensional flows in the Advanced Solid Rocket Motor (ASRM) and Redesigned Solid Rocket Motor (RSRM) are presented. In particular, a parametric study for the case of a gimballed nozzle in these motors at various burn times and gimbal angles is presented. The resultant pressure fields are used to determine the location of the center of pressure and hinge moments due to the internal flow of these geometries.
Document ID
19920023060
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reske, Edward J. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Billings, Dana F. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Cornelison, Joni W. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Publication Information
Publication: NASA. Goddard Space Flight Center, Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, Part 1
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
92N32304
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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