Abstract The technology of propulsive systems draws on a substantial body of formal fluid mechanical theory. The design of exhaust nozzles, turbine and compressor blade cascades, the analysis of the design-point operation of subsonic and supersonic inlets, etc., involve mathematically sophisticated solutions of the fluid motion and aero-thermochemical coupling between it and the medium. As difficult as some of these problems are, their basic formulation is usually reasonable clear. With enough effort, a theoretical framework can be developed and extended by controlled experimental work.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Interaction Flows Due to Supersonic Secondary Jets


    Beteiligte:


    Erscheinungsdatum :

    01.01.1968


    Format / Umfang :

    21 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






    Penetration of Gaseous Jets In Supersonic Flows

    Portz, Ron / Segal, Corin | AIAA | 2006


    Penetration of Gaseous Jets in Supersonic Flows

    Ron Portz / Corin Segal | AIAA | 2006


    NUMERICAL INVESTIGATION OF THE INTERACTION OF OPPOSING JETS AND SUPERSONIC FREE FLOWS

    Liu, Z.K. / Liu, Y.L. / Li, Q.Z. et al. | DataCite | 2024