Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Design of a Swept Wing Wind Tunnel Model for Study of Cross-flow Instability (AIAA 2015-2576)


    Contributors:

    Conference:

    Applied aerodynamics ; 2015 ; Dallas, TX



    Publication date :

    2015-01-01


    Size :

    15 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Two-Dimensional/Infinite Swept Wing Ice Accretion Model (AIAA 2015-0535)

    Bourgault-Cote, Simon / Laurendeau, Eric | British Library Conference Proceedings | 2015


    Wind Tunnel Flutter Testing of a Highly Swept All-Movable Wing (AIAA 2016-1960)

    Pitt, Dale M. / Sexton, Bradley / Byun, Kwanhwa | British Library Conference Proceedings | 2016


    Aeroservoelastic Wind-Tunnel Test of the SUGAR Truss Braced Wing Wind-Tunnel Model (AIAA 2015-1172)

    Scott, Robert C. / Allen, Timothy / Castelluccio, Mark et al. | British Library Conference Proceedings | 2015


    Variable Camber Compliant Wing - Wind Tunnel Testing (AIAA 2015-1051)

    Marks, Christopher R. / Zientarski, Lauren / Culler, Adam J. et al. | British Library Conference Proceedings | 2015