The influence of centerline and the cross-section variation to aerodynamic performance of the inlet was researched in a wider range. A new method of measuring the total pressure recovery coefficient and total pressure distortion coefficient of the inlet was proposed. Based on the loitering aircraft, a s-shaped inlet was designed to meet the needs of stable flight of loitering aircraft, whose total pressure recovery coefficient is 93.2% and total pressure distortion coefficient is 1.2%.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Design of S-Shaped Submerged Inlet



    Erschienen in:

    Advanced Materials Research ; 291-294 ; 349-354


    Erscheinungsdatum :

    04.07.2011


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






    Automated Design Optimization of a Submerged Inlet

    Taskinoglu, Ezgi / Jovanovic, Vasilije / Elliot, Greg et al. | AIAA | 2003



    Automated Design Optimization of a Subsonic Submerged Inlet

    Taskinoglu, Ezgi / Jovanovic, Vasilije / Knight, Doyle et al. | AIAA | 2004