Accession Number:

AD0648151

Title:

DRAG PLATE BALANCE,

Descriptive Note:

Corporate Author:

ATMOSPHERIC SCIENCES LAB WHITE SANDS MISSILE RANGE N MEX

Personal Author(s):

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

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE