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Characterization, parameter estimation, and aircraft response statistics of atmospheric turbulenceA nonGaussian three component model of atmospheric turbulence is postulated that accounts for readily observable features of turbulence velocity records, their autocorrelation functions, and their spectra. Methods for computing probability density functions and mean exceedance rates of a generic aircraft response variable are developed using nonGaussian turbulence characterizations readily extracted from velocity recordings. A maximum likelihood method is developed for optimal estimation of the integral scale and intensity of records possessing von Karman transverse of longitudinal spectra. Formulas for the variances of such parameter estimates are developed. The maximum likelihood and least-square approaches are combined to yield a method for estimating the autocorrelation function parameters of a two component model for turbulence.
Document ID
19810023596
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mark, W. D.
(Bolt, Beranek, and Newman, Inc. Cambridge, MA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1981
Publication Information
Publisher: NASA
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-3463
BBN-4319
Report Number: NASA-CR-3463
Report Number: BBN-4319
Accession Number
81N32139
Funding Number(s)
CONTRACT_GRANT: NAS1-14837
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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