Analysis of aeroelastic stability of helicopter rotor automated. Symbolic-manipulation program, HESL, written in FORTRAN, used to aid in derivation of government equations of motion for elastic-bladed rotor. Operates both on expressions and matrices. By transferring some burden of algebraic manipulations from human analyst to computer, program reduces tedium analysis and conequent opportunity for errors.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Computerized Analysis Of Helicopter-Rotor Aeroelasticity


    Contributors:

    Published in:

    Publication date :

    1988-11-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Transonic Aeroelasticity Analysis For Helicopter Rotor Blade

    Chang, I-Chung / Gea, Lie-Mine / Chow, Chuen-Yen | NTRS | 1991


    APPLICATION OF COMPUTATIONAL AEROELASTICITY TO DESIGN OF HELICOPTER ROTOR BLADES

    Righi, M. / International Council of the Aeronautical Sciences; Optimage Ltd | British Library Conference Proceedings | 2010


    Computerized projection of helicopter rotor

    Ле Тхе Шон / Л. В. Пономаренко | DOAJ | 2000

    Free access


    Application of an Unsteady Aerodynamic Model to Helicopter Rotor Blade Aeroelasticity

    Narkiewicz, J. P. / Done, G. T. | British Library Conference Proceedings | 1995