Factors in design of range of light hovercraft with good performance for overwater and overland use (military, naval, government), with specific reference to HC6B and HC6C; reduction in skirt wear is achieved in HC6B by exceptional power/weight ratio in lift mode and improved cushion retention, former by utilizing engines producing 0. 9 bhp/lb (excluding heat exchanges and fans) allied to lightweight body construction and latter by aerodynamic means; skirt drag is further reduced by inducing peripheral jet to Coanda directly under inflated Coanda tubes; cutaway drawing, and table of particulars for both craft are included.


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    Titel :

    Design philosophy


    Weitere Titelangaben:

    Hovering Craft Hydrofoil


    Beteiligte:
    Hawker, A.E. (Autor:in)

    Erschienen in:

    Hovering Craft and Hydrofoil ; 5 , n 9-10 ; p 28-32


    Erscheinungsdatum :

    1966


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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