AERO 3101 Midterm: Exam-AERO3101-2004April

• School: Carleton University
• Department: Aerospace Engineering
• Course: AERO 3101
• Professor: All

Document Summary

Students must count the nurrber of pages in this examination"question paper before beginning to write, and report any discrepancy immediately to a proctor. T h i s e x a m i n a t i o n q u e s t i o n p a p e r m a y be taken from the examination room. Using the unit load method and considering only bending action, (a) (b) determine the horizontal deflection at d; and determine the rotalion at c in terms of ei, l andp,. t*-l. A p r i l 2 0 0 4. The uniform beam is simply supported at one end and by two springs, one with stiffness ft and the other, 2k, at the locations shown in figure q2 . The magntui" of k is such that k: ei/l3, where elis the flexural rigidity of the beam.