Method based on valuation of parasite resistance, wing or cell characteristics, and knowledge of engine propeller behavior, is intended for routine calculations; performance calculation includes maximum speed, stalling speed and service ceiling rate of climb at sea level and specified altitudes; climb in 10 min., time to climb to various altitudes, best speeds of climb, endurance at full throttle, range at full throttle, endurance at maximum range.
Practical airplane performance calculations
Aeronautical Eng. (A.S.M.E. Trans.)
1930
18 pages
48 Figs.
Aufsatz (Zeitschrift)
Englisch
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