Torsional response of stiffened circular composite spar

보강된 복합재 원형 스파의 비틀림 거동

Kim, Sung Joon;Lee, Donggeon

  • Received : 2019.03.07
  • Accepted : 2019.03.27
  • Published : 2019.03.31


To reduce the structural weight, thin-walled circular composite tube has been used as a main spar of high altitude-long endurance unmanned air vehicle(HALE UAV). Predicting the torsional response of stiffened circular spar is complex due to the inhomogeneous nature of section properties, which are dependent on fiber architecture and constituent material properties. The stiffener were placed in the top and bottom sectors of a tube to increase the torsional capabilities such as the rigidity and buckling strength. Numerical simulations were performed to estimate the effect of the stiffener on the torsional capacities. A static experimental test was performed on a stiffened tube, and the test results were compared with a numerical model. The numerical models showed good correlation and demonstrated the ability to predict the torsional capacity. Results presented herein will exhibit the effectiveness of stiffener on torsional strength and stiffness.


HALE UAV;Composite spar;Torsional response;Buckling strength;Torsional test