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)


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    Title :

    Practical Aerodynamics of the Yak-40 Aircraft


    Contributors:

    Publication date :

    1976


    Size :

    225 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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