24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-5.4.4


STRAIN GAGE LOADS CALIBRATION PARAMETRIC STUDY

W. A. Lokos, R. Stauf*
NASA Dryden Flight Research Center, USA; *Spiral Technology Inc., USA

Keywords: calibration parametric study, loads calibration optimization, loads calibration test, loads test design, strain-gage calibration

Documents a parametric study of various aircraft strain-gage load calibration test features that affect the quality of the resultant derived load equations. The effects of the following are compared: single-point and distributed loading, variation in applied test load magnitude, number of applied load cases, and wing-box-only compared with control-surface loading.


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