The internal performance characteristics of Highly Integrated Deployable Exhaust Nozzles (HIDEN) applicable to advanced short take-off and vertical landing aircraft have been investigated. Four nozzle concepts, designed for fan and core flow installations, were tested with varying contraction ratio and nozzle exit plane shape. In addition, two offtake duct designs, along with several centerbody and blocker geometries were tested to evaluate their effect on the static thrust and flow performance. This investigation was conducted in the static test facility of the NASA Langley 16-Foot Transonic Tunnel. A six-component strain-gage balance collected force and moment data, and static pressure, total pressure, and total temperature measurements were also made internal to the model. Room temperature, dry high-pressure air was used to simulate jet exhaust. The results indicate that the internal performance of these HIDEN concepts is comparable to previously tested nozzle concepts designed for thrust vectoring about a bearing plane. This report presents the configuration design of the HIDEN concepts and the results of the internal performance testing.


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    Titel :

    Internal performance of Highly Integrated Deployable Exhaust Nozzles


    Beteiligte:
    Taylor, John G. (Autor:in) / Asbury, Scott C. (Autor:in) / Mason, Mary L. (Autor:in) / Lamb, Milton (Autor:in)

    Kongress:

    AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit ; 1993 ; Monterey, CA, United States


    Erscheinungsdatum :

    01.06.1993


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Internal performance of Highly Integrated Deployable Exhaust Nozzles

    TAYLOR, JOHN / ASBURY, SCOTT / MASON, MARY et al. | AIAA | 1993


    Internal performance of two-dimensional wedge exhaust nozzles

    Beale, William T / Povolny, John H | NTRS | 1957


    Aerodynamic studies for deployable nozzles

    VENABLES, A. / LARUELLE, G. / GARCIA, P. et al. | AIAA | 1985



    Locomotive exhaust nozzles

    Engineering Index Backfile | 1918