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Dual strain gage balance system for measuring light loadsA dual strain gage balance system for measuring normal and axial forces and pitching moment of a metric airfoil model imparted by aerodynamic loads applied to the airfoil model during wind tunnel testing includes a pair of non-metric panels being rigidly connected to and extending towards each other from opposite sides of the wind tunnel, and a pair of strain gage balances, each connected to one of the non-metric panels and to one of the opposite ends of the metric airfoil model for mounting the metric airfoil model between the pair of non-metric panels. Each strain gage balance has a first measuring section for mounting a first strain gage bridge for measuring normal force and pitching moment and a second measuring section for mounting a second strain gage bridge for measuring axial force.
Document ID
19920000967
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Roberts, Paul W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
October 15, 1991
Subject Category
Instrumentation And Photography
Report/Patent Number
Patent Number: US-PATENT-5,056,361
Patent Application Number: US-PATENT-APPL-SN-584018
Patent Number: NASA-CASE-LAR-14419-1
Accession Number
92N10185
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,056,361|NASA-CASE-LAR-14419-1
Patent Application
US-PATENT-APPL-SN-584018
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