Considering aeroelastic effects plays a vital role in the aircraft design process. The construction of elastic wind tunnel models is critical element investigation occurring phenomena. However, structural scaling between full-scale and reduced-scale configurations complex manufacturing task usually avoided testing. This work proposes numerical approach for dynamic technique, which applied to fi...

An extensive experimental investigation to study the flow structure over the wing of a fighter type configuration model has been conducted. The model used for this study was similar to the High Alpha Research Vehicle (HARV) that has been used in various European research centers for studying its force and moment characteristics. Tests were conducted at two subsonic speeds and at low to moderate...