Review of design studies made to determine influence of aerodynamic parameters; basic assumptions or ground rules used; examination of power/weight and lift/drag ratio; effect of jet angles and thickness; design study on family of GEM's ranging from 25 to 400 tons; evaluation of design cushion pressure; dynamic stability over waves; economics.
Hovercraft -- Some design problems
Aerospace Eng
Aerospace Engineering ; 20 , n 2
1961
5 pages
Article (Journal)
English
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