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Mechanical Design of A Rotary Balance System for NASA - Langley's Vertical Spin TunnelA new, lightweight Rotary Balance System is presently being fabricated and installed as part of a major upgrade to the existing 20-Foot Vertical Spin Tunnel (Figure 1) located at NASA's Langley Research Center. This upgrade, to improve model testing productivity of the only free-spinning vertical wind tunnel in the Western Hemisphere, includes a modern fan/drive and tunnel control system, an updated video recording system, and the new rotary balance system. The rotary balance is a mechanical apparatus which enables the measurement of aerodynamic force and moment data under spinning conditions (100 rpm). This data is used in spin analysis and is vital to the implementation of large amplitude maneuvering simulations required for all new high performance aircraft. The present system is over 40 years old and is worn beyond acceptable tolerances, as well as being susceptible to frequent breakdowns. It has serious limitations in model weight, position adjustment and spin-rate capabilities.
The new rotary balance system described in this report will permit greater test efficiency and improved data accuracy. Rotary Balance testing with the model enclosed in a tare bag can also be performed to obtain resulting model forces from the spinning operation. The rotary balance system will be stored against the tunnel sidewall during free-flight model testing.
Document ID
19920015847
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
J. W. Allred
(Langley Research Center Hampton, United States)
V. J. Fleck
(Langley Research Center Hampton, United States)
Date Acquired
September 6, 2013
Publication Date
May 13, 1992
Publication Information
Publication: Proceedings of the 26th Aerospace Mechanisms Symposium
Publisher: National Aeronautics and Space Administration
Issue Publication Date: January 1, 1992
Subject Category
Research And Support Facilities (Air)
Meeting Information
Meeting: The 26th Aerospace Mechanisms Symposium
Location: Greenbelt, MD
Country: US
Start Date: May 13, 1992
End Date: May 15, 1992
Sponsors: Goddard Space Flight Center
Accession Number
92N25090
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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