The results of a study on rotary-balance testing for aircraft dynamics are presented. The study examined both the experimental techniques used to obtain rotary-flow aerodynamic data and the procedures involved in using this type of data in the mathematical modeling of the dynamic behavior of a maneuvering fighter aircraft. A special effort was made to summarize experiences involving correlation of dynamic behavior predictions with the observed motions of free-flight models and aircraft in flight. Specific hardware and problems encountered in rotary-balance experiments were addressed for experimental facilities in several countries and advanced applications were noted.


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    Title :

    Rotary-Balance Testing for Aircraft Dynamics (Les Essais sur Balance Rotative pour l'Etude de la Dynamique du Vol de l'Avion)


    Publication date :

    1990


    Size :

    267 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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