Accurate measurement of location where laminar boundary layer undergoes transition to turbulent one serves many purposes in basic aero-dynamic research and developmental testing. Individual gages must be staggered to prevent formation of turbulence at gages downstream. This arrangement precludes accurate measurements of laminar/turbulent transition regions along streamline. Complete understanding of performance, stability, and control of laminar-flow airplane requires knowledge of transition locations on wing surface, empennage surfaces, fuselage, and nacelles. Visual, acoustic, and electronic methods capable of providing this transition information.


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    Titel :

    Continuous, Multielement, Hot-Film Transition Gage


    Beteiligte:
    Holmes, B. (Autor:in) / Mcpherson, J. (Autor:in) / Harris, F. (Autor:in) / Diamond, J. (Autor:in) / Johnson, N. (Autor:in) / Chapman, J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1986-05-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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    The narrow gage, especially one-meter gage

    Engineering Index Backfile | 1925


    Crossflow vortex and transition measurements by use of multielement hot films

    Agarwal, Naval K. / Maddalon, Dal V. / Mangalam, Siva M. et al. | NTRS | 1992


    Multielement airfoil ice accretion

    Washington, Thomas / Drela, Mark | AIAA | 1995