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Low-Hysteresis Flow-Through Wind-Tunnel BalanceImproved flow-through wind-tunnel balance includes features minimizing both spurious force readings caused by internal pressurized flow and mechanical hysteresis. Symmetrical forces caused by internal flow cancelled.
Document ID
19920000095
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Kunz, N. (NASA Ames Research Center, Moffett Field, CA.)
Luna, P. M. (NASA Ames Research Center, Moffett Field, CA.)
Roberts, A. C. (NASA Ames Research Center, Moffett Field, CA.)
Smith, R. C. (NASA Ames Research Center, Moffett Field, CA.)
Horne, W. L. (Micro Craft, Inc.)
Smith, K. M. (Micro Craft, Inc.)
Date Acquired
August 15, 2013
Publication Date
February 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-11877
Accession Number
92B10095
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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