The starting characteristics for three different model geometries were tested in the Glenn Research Center 225 Square Centimeter Supersonic Wind Tunnel. The test models were tested at Mach 2, 2.5 and 3 in a square test section and at Mach 2.5 again in an asymmetric test section. The results gathered in this study will help size the test models and inform other design features for the eventual implementation of a magnetic suspension system.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Blockage Testing in the NASA Glenn 225 Square Centimeter Supersonic Wind Tunnel


    Beteiligte:

    Kongress:

    SciTech 2017 ; 2017 ; Grapevine, TX, United States


    Erscheinungsdatum :

    09.01.2017


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Blockage Testing in the NASA Glenn 225 Square Centimeter Supersonic Wind Tunnel

    Sevier, Abigail E. / Davis, David O. / Schoenenberger, Mark | AIAA | 2017


    Blockage Testing in the NASA Glenn 225 Square Centimeter Supersonic Wind Tunnel (AIAA 2017-1213)

    Sevier, Abigail E. / Davis, David O. / Schoenenberger, Mark | British Library Conference Proceedings | 2017


    Aerodynamic Testing Capabilities of the NASA Glenn 10- by 10-Foot Supersonic Wind Tunnel

    Arrington, Allen / Pastor, Christine / Simerly, Stephanie | AIAA | 2011


    AERODYNAMIC TESTING CAPABILITIES OF THE NASA GLENN 10- BY 10-FOOT SUPERSONIC WIND TUNNEL

    Arrington, A. / Pastor, C. / Simerly, S. et al. | British Library Conference Proceedings | 2011


    NASA Glenn Wind Tunnel Model Systems Criteria

    R. H. Soeder / J. W. Roeder / D. E. Stark et al. | NTIS | 2004