Weighing method described in which both fuel tank and comparative weight are suspended from springs not far from each other; in flight tests accurate readings were obtained at accelerations up to 3 g and positional changes of about 50°. Abstract from Luftfahrtforschung v 20 Oct 16 1943 p 263-7. (See also VDI Zeit v 88 n 3-4 Jan 22 1944 p 53; English abstracts in Engrs' Digest (British Edition) v 5 n 8 Aug 1944 p 223-5)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Fuel content gage for aircraft


    Additional title:

    Kraftstoff-Vorratsmesser fuer Flugzeuge


    Contributors:
    Czerlinsky, E. (author) / Zeyns, J. (author)


    Publication date :

    1944


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Fuel content gage for aircraft

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


    Fuel content gage for aircraft

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


    RADIATION FUEL GAGE APPLICATIONS TO TRANSPORT AIRCRAFT

    BURNAP, C. F. | SAE Technical Papers | 1961


    Radiation fuel gage applications to transport aircraft

    Burnap, C.F. | Engineering Index Backfile | 1961


    Flight test of nucleonic type aircraft fuel gage

    Harwick, B.T. / Hochheiser, J.S. | Engineering Index Backfile | 1966