Study of afterburner flameholder temperatures13;

Sridhara, K and Chidananda, MS and Isaac, JJ (1977) Study of afterburner flameholder temperatures13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Measurements of bluff body and aerodynamic flameholder13; under temperatures, under simulated afterburner13; conditions have been made. The effects of afterburner13; operating variables such as the Inlet Mach number,13; temperature and fuel-air ratio on measured flameholder13; temperatures have bees presented. It has been further demonstrated that, under identical operating the temperatures of the aerodynamic flameholder are than significantly less those of an equivalent V-guttor, while retaining identical, et ability .characteristics with the inherent advantage of a negligible dry pressure loss. Consequently* the aerodynamic flameholder will havxAB; a better operating life as compared to a bluff body flameholder, in addition to its other significant advantage.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Flameholder;V-gutter
    Subjects: AERONAUTICS > Aircraft Propulsion and Power
    Division/Department: Propulsion Division, Propulsion Division, Propulsion Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 13 Nov 2006
    Last Modified: 24 May 2010 09:53

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