| 摘要 |
A method for evaluating the structural compatibility of an aircraft for use on a runway having a profile with one or more roughnesses in the form of bumps and/or dips, comprising the steps of: generating a first bump height curve representing elevations or depressions on the runway; comparing the bump height curve with a second bump height curve which is a first reference curve; generating a first power spectral density curve of the profile of the runway; comparing the first power spectral density curve with a second power spectral density curve which is a second reference curve; authorizing or denying the aircraft the use of the runway on the basis of results of the comparison between the bump height curve and the first reference curve, and between the power spectral density curve and the second reference curve.
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