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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

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