Print Email Facebook Twitter Equations for the response of an airplane to non-stationary atmospheric turbulence patches Title Equations for the response of an airplane to non-stationary atmospheric turbulence patches Author Noback, R. Institution National Aerospace Laboratory NLR Date 1976-03-08 Abstract In this report a method is described to calculate the load exceedance curve for a linear system having a finite, modulated Gaussian process as input. The derivation is based on the use of ensemble averages, defined as the expected values at a certain point of time. The equations can be used for any airplane-transfer function for which the Power Spectral Density method is applicable. Subject gust loadsrandom loadsatmospheric turbulenceturbulencestatistical analysistransfer functionstransient responsestochastic processesaircraft designpower spectraexpectancy hypothesis To reference this document use: http://resolver.tudelft.nl/uuid:565f5002-5841-44c7-8a36-3c6b1ab43024 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 76056 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1976 National Aerospace Laboratory NLR Files PDF NLR_TR_76056_U.pdf 17.11 MB Close viewer /islandora/object/uuid:565f5002-5841-44c7-8a36-3c6b1ab43024/datastream/OBJ/view