Account of aerodynamic considerations involved in evolution of new executive or feederliner aircraft and basic design requirements; design specification selected for aircraft seating 6 to 10 executive passengers in comfort or 18 passengers, having range of 1500 mi stage with 5 executive passengers and luggage plus crew of 2, and cruising in 300 mph bracket; field length required is about 1000 yd; description of aircraft, choice of powerplant and propeller; aerodynamic design; schematics and various layouts.


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    Title :

    Aerodynamic design philosophy of handley page jetstream


    Additional title:

    Aircraft Eng


    Contributors:
    Lee, G.H. (author)

    Published in:

    Publication date :

    1967


    Size :

    12 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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