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Random harmonic analysis program, L221 (TEV156). Volume 1: Engineering and usageA digital computer program capable of calculating steady state solutions for linear second order differential equations due to sinusoidal forcing functions is described. The field of application of the program, the analysis of airplane response and loads due to continuous random air turbulence, is discussed. Optional capabilities including frequency dependent input matrices, feedback damping, gradual gust penetration, multiple excitation forcing functions, and a static elastic solution are described. Program usage and a description of the analysis used are presented.
Document ID
19800003808
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Miller, R. D.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Graham, M. L.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
D6-44466
NASA-CR-2857
Accession Number
80N12058
Funding Number(s)
CONTRACT_GRANT: NAS1-13918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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