Study of electrostatic phenomena during fueling of jet aircraft wing tank and small scale rig representing single compartment of integral wing tank, using batches of typical aviation turbine fuels; charge densities in fuel, electrostatic field strengths in vapor spaces of tanks, and occurrence of discharges were measured as functions of operating conditions; high field strengths were attained over wide range of operating conditions, resulting in discharges in many cases. (CRC Project CA-22-59)


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    Titel :

    Electrostatic discharges in aircraft fuel systems, phase 2


    Weitere Titelangaben:

    Electrostatic Discharges Aircraft Fuel Systems, Phase 2



    Erscheinungsdatum :

    1961


    Format / Umfang :

    83 pages


    Medientyp :

    Buch


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :