Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Acoustic Characteristics of Compressible Jet from Different Nozzle exit Geometry


    Contributors:

    Conference:

    25th AIAA/CEAS Aeroacoustics Conference



    Publication date :

    2019-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Surrogate Model-Based Acoustic Optimisation of Jet Nozzle Exit Geometry

    Yang, Guangda / Allen, Christian B. / Markesteijn, Annabel P. et al. | AIAA | 2022


    Aero-acoustic Characteristics of Compressible Jets from Chevron Nozzle

    Nikam, Shailesh R. / Sharma, Shailendra D. | AIAA | 2014


    Effects of Exit Nozzle Diameter on Compressible Vortex Rings Flow Structure

    Mariani, Raffaello / Kontis, Konstantinos | AIAA | 2009


    Effect of Nozzle Exit Geometry on Submerged Jet Characteristics in Underwater Propulsion

    Arghode, V. / Gupta, A. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008


    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