Discussion of question of performance and factors on which it depends, in order to justify numerical values given; if airplane can be produced, with gliding angle as low as 1 in 25, to "take-off" and fly at low altitude carrying half its gross weight in fuel, there is every prospect that half-circumference of earth, 12, 600 mi, may be covered in single flight without refueling. (See also - n 3840 Aug 18 1939 p 203-5)
Maximum range of flight
Engineering
Engineering ; 148 , n 3841
1939
3 pages
Aufsatz (Zeitschrift)
Englisch
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