Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Effects of Exit Nozzle Diameter on Compressible Vortex Rings Flow Structure


    Contributors:

    Conference:

    47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition ; 2009 ; Orlando , Florida



    Publication date :

    2009-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Effects of Exit Nozzle Diameter on Compressible Vortex Rings Flow Structure

    Mariani, R. / Kontis, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009


    Analysis of the Flow Dynamics of Compressible Vortex Rings Using Compressible Gases

    Mariani, R. / Kontis, K. / European Space Agency | British Library Conference Proceedings | 2009


    Acoustic Characteristics of Compressible Jet from Different Nozzle exit Geometry

    Nikam, Shailesh R. / Bhikole, Siddhesh / Suvagiya, Malay | AIAA | 2019



    Effects of nozzle exit geometry on forebody vortex control using blowing -

    Gittner, Nathan M. / Chokani, Ndaona | AIAA | 1994