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Dynamic-Loads Analysis of Flexible Aircraft With Active ControlsIntegrated system of stand-along computer programs, DYLOFLEX, analyzes dynamic loads on flexible aircraft with active controls. DYLOFLEX capabilities include calculating dynamic loads due to continuous atmospheric turbulence, discrete gusts, and discrete control inputs. Each of the eight individual DYLOFLEX programs may be used alone or in conjunction with other DYLOFLEX programs.
Document ID
19810000200
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Perry, B. I.
Durling, B. J.
Date Acquired
August 11, 2013
Publication Date
November 1, 1982
Publication Information
Publication: NASA Tech Briefs
Volume: 6
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12747
Accession Number
81B10200
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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