NASA's Advanced Subsonic Technology (AST) Program seeks to develop new technologies to increase the fuel efficiency of commercial aircraft engines, improve the safety of engine operation, and reduce emissions and engine noise. For new designs of ducted fans, compressors, and turbines to achieve these goals, a basic aeroelastic requirement is that there should be no flutter or high resonant blade stresses in the operating regime. For verifying the aeroelastic soundness of the design, an accurate prediction/analysis code is required. Such a three-dimensional viscous propulsion aeroelastic code, named TURBO-AE, is being developed at the NASA Lewis Research Center. The development and verification of the flutter version of the TURBO-AE code (version 4) has been completed. Validation of the code is partially complete.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Flutter Version of Propulsion Aeroelasticity Code Completed


    Contributors:

    Publication date :

    1999


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Dynamic Aeroelasticity – Flutter

    Wright, Jan R. / Cooper, Jonathan E. | Wiley | 2014


    Static Aeroelasticity and Flutter

    Wright, Jan R. / Cooper, Jonathan E. | Wiley | 2014



    Flutter control of aeroelasticity with freeplay nonlinearity

    Daochun, L. / Jinwu, X. | British Library Online Contents | 2007