The new wall pressure measurement system and the TWICS wall correction system for the 14x22-Ft subsonic tunnel are described. Results from a recent semispan test and a full-span test are presented. Comparison with existing classical methods of correction is shown. A modification of the TWICS code to treat the effect due to a deflected wake from a high-lift wing is also discussed. The current implementation of TWICS for the 14x22-Ft tunnel is shown to be an improvement over existing methods.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Improvements to Wall Corrections at the NASA Langley 14 x 22-Ft Subsonic Tunnel


    Beteiligte:
    Iyer, Venkit (Autor:in) / Kuhl, David D. (Autor:in) / Walker, Eric L. (Autor:in)

    Kongress:

    21st AIAA Applied Aerodynamics Conference ; 2003 ; Orlando, FL, United States


    Erscheinungsdatum :

    01.01.2003


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Improvements to Wall Corrections at the NASA Langley 14x22-Ft Subsonic Tunnel

    Iyer, Venkit / Kuhl, David / Walker, Eric | AIAA | 2003


    AIAA-2003-3950 Improvements to Wall Corrections at the NASA Langley 14x22-Ft Subsonic Tunnel

    Iyer, V. / Kuhl, D. / Walker, E. et al. | British Library Conference Proceedings | 2003


    Subsonic Wind Tunnel Wall Corrections

    W. E. Acum / H. C. Garner / E. C. Maskell et al. | NTIS | 1966


    Subsonic wind tunnel wall corrections

    Rogers, E. W. E. / Acum, W. E. A. / Maskell, E. C. et al. | TIBKAT | 1966