This design synopsis of aircraft hydraulic systems is intended to convey to designers computation data and information concerning applicable specifications. Design, installation and construction of the hydraulic systems in military aircraft is governed by Specification MIL-H-5440 (Hydraulic Systems; Design, Installation and Tests of Aircraft) and a large number of detail specifications referenced therein. These specifications are not mandatory for commercial aircraft but the wise designer will use them unless they involve a severe weight or cost penalty. (Author)


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    Title :

    Design Synopsis Aircraft Hydraulic Systems


    Contributors:
    H. Field (author)

    Publication date :

    1952


    Size :

    39 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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