抄録
Experimental results are presented on 30 test piecies of Wide-flange rolled shape members under biaxial bending and thrust load. In all the tests the ends of members were pinned and heavy plates were used to restrain warping. Two basic cross sections (H-100×100×100×6×8, H-150×100×6×9) were used as test members and slenderness ratios were varied from 20 to 40, . Loading conditions were selected as axial thrust load ratios P/P_y=0.2, 0.4, and moment ratio about two axis m_1/m_2=0, 0.6, and 1.0, . Load-deflection curves are shown comparing with numerical results by the analytical method described in the previous report (Part I). There are good agreements between test and analytical results.
