A limited calibration of a combined pitot-static tube and vane-type flow-angularity indicator has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.61 and 2.01. The results indicated that the angle-of-yaw indications were affected by unsymmetric shock effects at low angles of attack.


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    Titel :

    Wind-tunnel calibration of a combined pitot-static tube and vane-type flow-angularity indicator at Mach numbers of 1.61 and 2.01


    Beteiligte:

    Erscheinungsdatum :

    01.10.1956


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch