The technology data base for powered lift aircraft design has advanced over the last 15 years. NASA's Quiet Short Haul Research Aircraft (QSRA) has provided a flight verification of upper surface blowing (USB) technology. The A-6 Circulation Control Wing flight demonstration aircraft has provide data for circulation control wing (CCW) technology. Recent small scale wind tunnel model tests and full scale static flow turning test have shown the potential of combining USB with CCW technology. A flight research program is deemed necessary to fully explore the performance and control aspects of CCW jet substitution for the mechanical USB Coanda flap. The required hardware design would also address questions about the development of flight weight ducts and CCW jets and the engine bleed-air capabilities vs requirements. NASA's QSRA would be an optimum flight research vehicle for modification to the USB/CCW configuration. The existing QSRA data base, the design simplicity of the QSRA wing trailing edge controls, availability of engine bleed-air, and the low risk, low cost potential of the suggested program is discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Potential Flight Evaluation of an Upper-Surface-Blowing/Circulation-Control-Wing Concept


    Beteiligte:
    D. W. Riddle (Autor:in) / J. C. Eppel (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    29 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Noise from a circulation control wing with upper surface blowing

    Salikuddin, M. / Brown, W.H. / Ahuja, K.K. | Tema Archiv | 1985


    Noise from a circulation control wing with upper surface blowing

    SALIKUDDIN, M. / BROWN, W. / AHUJA, K. | AIAA | 1985


    Noise from a circulation control wing with upper surface blowing

    SALIKUDDIN, M. / BROWN, W. H. / AHUJA, K. K. | AIAA | 1987