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Improved Stability and Control Analysis Process for Detailed Design Stage of Light Aircraft
Le Viet Thang Nguyen,Nhu Van Nguyen,Jae-Woo Lee,Sangho Kim,Seung-Hyeog Nah 한국항공우주학회 2016 한국항공우주학회 학술발표회 논문집 Vol.2016 No.4
The improved stability and control (S&C) analysis process is developed and presented using wind tunnel test data to investigate the stability and control characteristics of a light aircraft complied with the KAS – VLA subpart B regulations and design requirements at detailed design stage. The enhanced stability and control analysis disciplines are developed for the corresponding KAS – VLA regulations and design requirements to use wind tunnel (W/T) test data, weight and propulsion data in order to improve the reliability of stability and control analysis results. In this study, the improved S&C process is applied for detailed design stage of light aircraft and complied with KAS – VLA to demonstrate the efficiency of the process.