NASA Technical Paper 2256 - CAFE Foundation
NASA Technical Paper 2256 - CAFE Foundation
NASA Technical Paper 2256 - CAFE Foundation
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APPENDIX<br />
base. Becauseof these shortcomings in the dial indicator methodof waviness measurement,<br />
the data are defined as "indicated" waviness.<br />
The indicated waviness data measuredon the airplanes tested are presented in<br />
figures A2 through A7. Table AI is a summaryof the waviness data in terms of the<br />
numberof waves at each location and the chordwise position, double amplitude, and<br />
wavelengths of the largest wave in * _e laminar region and over the total chord at<br />
each spanwise measurement location. Only waves that were-2 in. or shorter were<br />
counted; most waves fell in this category. Waves which occurred in the turbulent<br />
region of the chord were included in the table as an indication of-overall surface<br />
quality. The maximum allowable multiple wave heights are also given in table AI. A<br />
comparison between the maximum measured and maximum allowable wave heights shows that<br />
the waves existing in the laminar region of all but one of the test airplanes were<br />
smaller than allowable for premature transition.<br />
29<br />
l