Equations developed for correction of level speed and rate of climb for variation of air temperature and aircraft weight, applicable to aircraft with engines driving propellers operating at speeds sufficiently high for compressibility effects on drag and propeller efficiency to be appreciable; practical applications of equations.
General performance reduction equations for reciprocating-engined aircraft with constant-speed propellers
Aeronautical Quarterly
Aeronautical Quarterly ; 2 , Part 2
1950
16 pages
Article (Journal)
English
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