Subsonic transports; influence of size on aircraft economics and compromise between cruising efficiency and tractable approach and landing characteristics; subsonic speed/height and direct operating cost patterns shown; factors associated with flight in supersonic region Mach 1.0 to 5.0 considering engines, aerodynamics and structures; economics and operation with respect to size of fleet, traffic potential and costs; supersonic long range transports; noise problems and traffic control. (See also - discussion p 326-34)
Supersonic aircraft -- Promise and problems
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 64 , n 594
1960
12 pages
Article (Journal)
English
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