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Accession Number:
AD0648151
Title:
DRAG PLATE BALANCE,
Descriptive Note:
Corporate Author:
ATMOSPHERIC SCIENCES LAB WHITE SANDS MISSILE RANGE N MEX
Report Date:
1966-12-01
Pagination or Media Count:
31.0
Abstract:
The paper discusses the design features of a proposed drag plate for the ASO low speed wind tunnel at White Sands Missile Range, New Mexico. The device will measure the chord force exerted on an object mounted flush atop the drag plate by the use of an external strain gage balance. The required readout system for the drag plate is given. Author
Distribution Statement:
APPROVED FOR PUBLIC RELEASE