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MEASUREMENT OF THE ROLLING MOMENT ON AIRCRAFT MODELS 2013 COBISS.BH-ID 4069656, ISBN 978-99955-26-32-0 http://ezaposleni.singidunum.ac.rs/rest/sciNaucniRezultati/oai/record/1/1808 M. Samardžić D. Regodić Z. Anastasijević D. Marinkovski Measurement of aerodynamic load on the aircraft and missile models is one of the main tasks in wind tunnel testing. Aerodynamic load on the wind tunnel models can be measured using internal or external wind tunnel balances. Wind tunnel balances resolve the total aerodynamic load into a number of components (generally between three and six). In this paper two ways of the rolling moment measurement is presented: measurement of the rolling moment using the proper measuring element with one bar and measurement of the rolling moment using five-bar measuring element. Measuring elements are realized as strain gauge transducers. conferenceObject 304 309 339:327(082); 316.32 ; 811 Zbornik radova [Електронски извор] / XIV; Univerzitet Sinergija, 2013 (Studio Avalon : CD izdanje). - 1 elektronski optički disk (CD-ROM)