The structural and aerodynamic properties of the Yak-40 passenger aircraft and its technical flight characteristics are presented. The problems of flying techniques are discussed and specific recommendations are given for executing flight under various conditions. Information is presented about the equilibrium, stability and controllability, flight in specific situations, flying the aircraft with engine cutout and in turbulent air. Some propositions are also given from the theory of flight, which simplify the study of the problems of practical aerodynamics and flight operation. (Author)
Practical Aerodynamics of the Yak-40 Aircraft
1976
225 pages
Report
No indication
English
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