Abstract Algorithms for calculating superlight aircraft design parameters at the early stage of design are described, namely, maximum speed, time of landing or takeoff run, of maneuvering with well-known piston engine power and propeller characteristics.
Algorithms for calculating some flight characteristics and design parameters of a superlight piston-engined aircraft
Russian Aeronautics (Iz VUZ) ; 52 , 1 ; 99-103
2009-03-01
5 pages
Article (Journal)
Electronic Resource
English
Design calculation of superlight piston-engined aircraft flight characteristics
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