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Aeolian processes aboard a space station: Saltation and particle trajectory analysisThe Carousel wind tunnel (CWT) proposed to study aeolian processes aboard a space station consists of two concentric rotating drums. The space between the two drums comprises the wind tunnel test section. Differential rates of rotation of the two drums would provide a wind velocity with respect to either drum surface. Preliminary results of measured velocity profiles made in a CWT prototype indicate that the wall bounded boundary layer profiles are suitable to simulate flat plate turbulent boundary layer flow. The two dimensional flat plate Cartesian coordinate equations of motion of a particle moving through the air are explained. In order to assess the suitability of CWT in the analysis of the trajectories of windblown particles, a series of calculations were conducted comparing cases for gravity with those of zero gravity. Results from the calculations demonstrate that a wind tunnel of the carousel design could be fabricted to operate in a space station environment and that experiments could be conducted which would yield significant results contributing to the understanding of the physics of particle dynamics.
Document ID
19860017693
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
White, B. R.
(California Univ. Davis, CA, United States)
Greeley, R.
(Arizona State Univ. Tempe, United States)
Iversen, J. D.
(Iowa State Univ. of Science and Technology, Ames, United States)
Leach, R. N.
(Santa Clara Univ. Calif., United States)
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Publication Information
Publication: NASA. Lyndon B. Johnson Space Center Space Station Planetology Experiments (SSPEX)
Subject Category
Research And Support Facilities (Air)
Accession Number
86N27165
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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