Performance of a cobra probe and an asymmetric probe in a cascade tunnel

Manickam, MD and Mahalingam, S (1973) Performance of a cobra probe and an asymmetric probe in a cascade tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Full text available as:
[img] PDF
Restricted to Archive staff only

Download (713Kb)

    Abstract

    A three - tube cobra type probe and an asymmetric three - tube probe have been used in subsonic cascade tunnel for the measurement of wake profile and a quantitative comparison of their performance is made.In the case of the cobra probe, a little variation in the flow direction13; is observed during wake traverse due to the presence of the total pressure gradient in the plane containing the yaw sensing elements.The average outlet angle measured by an asymmetric probe is about 3.0 degrees more than the average angle measured by a cobra - type probe. However the values of the total pressure loss and the absolute outlet velocity are found to be very much the same in both cases.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Asymmetric tube;Subsonic cascade
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Propulsion Division, Propulsion Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 09 Nov 2006
    Last Modified: 24 May 2010 09:53
    URI: http://nal-ir.nal.res.in/id/eprint/3319

    Actions (login required)

    View Item