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    Titel :

    Development of a New Boundary Layer Control Technique for Automotive Wind Tunnel Testing (AIAA 2006-0356)



    Kongress:

    44th, Aerospace sciences meeting: a collection of technical papers; Vol 6 ; 2006 ; Reno, NV



    Erscheinungsdatum :

    2006-01-01


    Format / Umfang :

    10 pages


    Anmerkungen:

    Vol 6 of 23. See also m06/23197 � m06/23220



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    DEVELOPMENT OF A NEW BOUNDARY LAYER CONTROL TECHNIQUE FOR AUTOMOTIVE WIND TUNNEL TESTING

    Farrell, T. E. / Miller, L. S. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2006



    Preliminary Wind Tunnel Testing of WWI Fighters (AIAA 2006-0333)

    Eberhardt, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006


    Traveling Crossflow Wave Predictions on the HIFiRE-5 at Mach 6: Stability Analysis vs. Quiet Tunnel Data (AIAA 2016-0356)

    Lakebrink, Matthew T. / Borg, Matthew P. | British Library Conference Proceedings | 2016


    The Effect of Groundplane Boundary Layer Control on Automotive Testing in a wind Tunnel

    Berndtsson, A. / Mercker, E. / Eckert, W. T. | SAE Technical Papers | 1988