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Static and Dynamic Force/Moment Measurements in the Eidetics Water TunnelWater tunnels have been utilized in one form or another to explore fluid mechanics and aerodynamics phenomena since the days of Leonardo da Vinci. Water tunnel testing is attractive because of the relatively low cost and quick turn-around time to perform flow visualization experiments and evaluate the results. The principal limitation of a water tunnel is that the low flow speed, which provides for detailed visualization, also results in very small hydrodynamic (aerodynamic) forces on the model, which, in the past, have proven to be difficult to measure accurately. However, the advent of semi-conductor strain gage technology and devices associated with data acquisition such as low-noise amplifiers, electronic filters, and digital recording have made accurate measurements of very low strain levels feasible. The principal objective of this research effort was to develop a multi-component strain gage balance to measure forces and moments on models tested in flow visualization water tunnels. A balance was designed that allows measuring normal and side forces, and pitching, yawing and rolling moments (no axial force). The balance mounts internally in the model and is used in a manner typical of wind tunnel balances. The key differences between a water tunnel balance and a wind tunnel balance are the requirement for very high sensitivity since the loads are very low (typical normal force is 0.2 lbs), the need for water proofing the gage elements, and the small size required to fit into typical water tunnel models.
Document ID
19950007824
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Carlos J Suarez
(Eidetics Aircraft Torrance, California, United States)
Gerald N Malcolm
(Eidetics Aircraft Torrance, California, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Publication Information
Publication: Fourth High Alpha Conference: Volume 1
Publisher: National Aeronautics and Space Administration
Volume: 1
Subject Category
Aerodynamics
Report/Patent Number
NASA-CP-10143-VOL-1
Meeting Information
Meeting: 4th High Alpha Conference
Location: Edwards, CA
Country: US
Start Date: July 12, 1994
End Date: July 14, 1994
Sponsors: National Aeronautics and Space Administration
Accession Number
95N14238
Funding Number(s)
CONTRACT_GRANT: NAS2-13571
Distribution Limits
Public
Copyright
Public Use Permitted.
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