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.
Dynamic-Loads Analysis of Flexible Aircraft With Active Controls
NASA Tech Briefs ; 6 , 2
1982-11-01
Miscellaneous
No indication
English
Design Landing Loads Evaluation by Dynamic Simulation of Flexible Aircraft
British Library Conference Proceedings | 1991
|Dynamic Aircraft Model with Active Winglet, Effects of Flight Mechanics and Loads Analysis
Springer Verlag | 2015
|Active controls in aircraft design
NTRS | 1978
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