Several tests were performed on a one-sixth scale Rocket Based Combined Cycle (RBCC) engine model at the University of Alabama in Huntsville. The UAH RBCC facility consists of a rectangular duct with a vertical strut mounted in the center. The scaled strut consists of two supersonic rocket nozzles with an embedded vertical turbine between the rocket nozzles. The tests included mass flow, flow visualization and horizontal pressure traverses. The mass flow test indicated a c:hoked condition when the rocket chamber pressure is between 200 psi and 300 psi. The flow visualization tests narrowed the rocket chamber pressure range from, 250 psi to 300 psi. Also, from this t.est, an assumption of a minimum


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    Titel :

    Investigation of the Rocket Induced Flow Field in a Rectangular Duct


    Beteiligte:
    Landrum, D. Brian (Autor:in) / Thames, Mignon (Autor:in) / Parkinson, Doug (Autor:in) / Gautney, Serena (Autor:in) / Hawk, Clark (Autor:in)

    Kongress:

    Joint Propulsion ; 1999 ; Los Angeles, CA, United States


    Erscheinungsdatum :

    1999-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Investigation of the Rocket Induced Flow Field in a Rectangular Duct

    Landrum, D. Brian / Lambert, James / Thames, Mignon et al. | NTRS | 1999


    Investigation of the Rocket Induced Flow Field in a Rectangular Duct

    D. B. Landrum / J. Lambert / M. Thames et al. | NTIS | 1999


    Investigation of the rocket induced flow field in a rectangular duct

    Landrum, D. / Thames, Mignon / Parkinson, Doug et al. | AIAA | 1999



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    McLellan, C.H. / Bartlett, Jr., W.A. | Engineering Index Backfile | 1941