NASA NTRS · 19810000200
Dynamic-Loads Analysis of Flexible Aircraft With Active Controls
Abstract
Integrated 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.
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Perry, B. I., Durling, B. J.. 1982-11-01. Dynamic-Loads Analysis of Flexible Aircraft With Active Controls. https://ntrs.nasa.gov/citations/19810000200
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