A flight-loads measurement program on the YF-12 aircraft required the mounting of 101 strain-gauge bridges in the fuselage, fuel tanks, control surfaces, and three stations on the left wing. The sensors were to be installed primarily on titanium and were required to operate between -70 and +600 F. Strain gauges with modified Karma filaments and backings of glass-fiber reinforced epoxy resin matrices were selected and were installed with an epoxy adhesive. Attention is given to the calibration, mounting, and performance of the sensors in flight-load measurements.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Strain gage installation on the YF-12 aircraft.


    Beteiligte:
    Wilson, E. J. (Autor:in)

    Kongress:

    Spring Meeting ; 1973 ; Los Angeles, CA


    Erscheinungsdatum :

    01.05.1973


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Strain Gage

    NTIS | 1995


    Numerical Strain Gage Representation

    Nichol, K. / AIAA; ASME; ASCE | British Library Conference Proceedings | 1998


    A balloon strain gage

    RAND, J. | AIAA | 1981


    Fuel content gage for aircraft

    Czerlinsky, E. / Zeyns, J. | Engineering Index Backfile | 1944