Transonic mach number sweep system for the NAL 4'x4' trisonic wind tunnel

Srikantan, KV (1975) Transonic mach number sweep system for the NAL 4'x4' trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    This note describes the design of Transonic Mach Number Sweep system meant to vaxy the Mach number during a b1owdown in the Transonic range (M = 0.8 to 1.40). Mach number steps are achieved by preset controlled operation of Transonic Control13; Flaps. The stepwise increase in Mach number is obtained through divergence of the flaps and vice versa.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Transonic mach number
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 30 Aug 2006
    Last Modified: 24 May 2010 09:50
    URI: http://nal-ir.nal.res.in/id/eprint/2606

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