Engine developed by D.Napier and Son, derivative of which is to power Fairey Rotodyne helicopter, develops at takeoff 3000 ehp for net dry weight of 1575 lb and frontal area of 7.1 sq ft, with specific fuel consumption of 0.624 lb per ehp per hr; performance data; illustrations. (See also Engineering v 178 n 4617 July 23 1954 p 121-123; Flight v 66 n 2374 July 23 1954 p 113-8; Engineer v 198 n 5139 July 23 1954 p 115-8)


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    Title :

    "Eland" turbo-propeller engine


    Additional title:

    Aeroplane


    Published in:

    Aeroplane ; 87 , n 2244


    Publication date :

    1954


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    "Eland" turbo-propeller engine

    Engineering Index Backfile | 1954


    "Eland" turbo-propeller engine

    Engineering Index Backfile | 1954


    "Eland" turbo-propeller engine

    Engineering Index Backfile | 1954


    Napier "Eland"

    Penn, A.J. | Engineering Index Backfile | 1955


    Napier "Eland"

    Penn, A.J. | Engineering Index Backfile | 1955