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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    Titel :

    Dynamic-Loads Analysis of Flexible Aircraft With Active Controls


    Beteiligte:
    Perry, B. I. (Autor:in) / Durling, B. J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1982-11-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    DYLOFLEX: A Computer Program for Flexible Aircraft Flight Dynamic Loads Analyses with Active Controls

    Boyd Perry Richard I. Kroll / Ronald D. Miller / Robert C. Goetz | AIAA | 1980


    Design Landing Loads Evaluation by Dynamic Simulation of Flexible Aircraft

    Ghiringhelli, G. L. / Boschetto, M. / North Atlantic Treaty Organization; Advisory Group for Aerospace Research and Development; Structures and Materials Panel | British Library Conference Proceedings | 1991


    Dynamic Aircraft Model with Active Winglet, Effects of Flight Mechanics and Loads Analysis

    Kanakis, Toni / Prananta, Bimo / van Tongeren, Hans et al. | Springer Verlag | 2015



    Active controls in aircraft design

    Kurzhals, P. R. | NTRS | 1978