The problem of aerodynamic force measurements was dealt with. Multicomponent strain gaps were used in determining these forces. The measurement of wing and tailplane loads on a semimodel of the European Airbus A 300 B was reported. Interference effects of a slender wing-body configuration were experimentally determined. Hinge moments, rudder, and fin loads of a horizontal tail surface with a rudder were examined. The tail drag of an aircraft was determined in a transonic wind tunnel. Aerodynamic interference forces were analyzed by splitting up a model in several parts. Tail assemblies of missiles were investigated.


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    Titel :

    Force Measurements on Parts of Wind Tunnel Models


    Erscheinungsdatum :

    1975


    Format / Umfang :

    198 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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