Expressions developed for max range for three cruise flight conditions: constant altitude, varying altitude below 35,000 ft, and varying altitude above 35,000 ft; max range obtained by increasing cruising altitude as fuel is consumed; airplane configurations derived which correspond to aerodynamic optima for cruise conditions investigated; importance of thrust loading. (See also - discussion n 6 June p 341-2)
Range performance of turbojet airplanes
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 15 , n 2
1948
5 pages
Aufsatz (Zeitschrift)
Englisch
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