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Design and calibration of the carousel wind tunnelIn the study of planetary aeolian processes the effect of gravity is not readily modeled. Gravity appears in the equations of particle motion along with interparticle forces but the two terms are not separable. A wind tunnel that would permit variable gravity would allow separation of the forces and aid greatly in understanding planetary aeolian processes. The design Carousel Wind Tunnel (CWT) allows for a long flow distance in a small sized tunnel since the test section is a continuo us circuit and allows for a variable pseudo gravity. A prototype design was built and calibrated to gain some understanding of the characteristics of the design and the results presented.
Document ID
19860017682
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Leach, R. N.
(Arizona State Univ. Tempe, AZ, United States)
Greeley, R.
(Arizona State Univ. Tempe, AZ, United States)
Iversen, J.
(Iowa State Univ. of Science and Technology, Ames, United States)
White, B.
(California Univ. Davis., United States)
Marshall, J. R.
(Arizona State Univ. Tempe, AZ, 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
86N27154
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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