The classical theory of range performance is reviewed, and some further relationships derived. The specific range, which is the instantaneous range performance of an aircraft at a point on a cruise trajectory, in terms of distance covered per unit quantity of fuel consumed is considered. The integration of specific range over a given flight trajectory, to give the integral range on a given quantity of fuel is also discussed, and comparisons are made between the ranges obtained using various cruising techniques. (Author)
Range Performance in Cruising Flight
1974
58 pages
Report
No indication
English
Range Performance in Cruising Flight
NTIS | 1974
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