Simulations of pressure transients are obtained for tanker aerial refueling systems during tanker disconnects from receiver aircraft using a fluid transient analysis computer program. Effects of tanker nozzle valve closure characteristics on transient pressures are described. The results are compared with experimental results reported in the literature. Reasonable agreement is obtained.


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    Title :

    Pressure Transients in Aerial Refueling Systems


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Aerospace Congress and Exposition ; 1983



    Publication date :

    1983-10-03




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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