TASK-BASED ASSESSMENT IN THE ALBANIAN CONTEXT
Task-based assessment is timely, because issues of critical thinking and lifelong learning have come to the fore in discussions of the national educational reform. TBA is of increasing interest to teachers and educators, because of its emphasis on active, transferable learning, its potential for motivating students to develop problem-solving skills and in becoming effective collaborators. TBA has been widely explored and studied by many researchers in the field of English language teaching. However, there are few or no official studies that specifically deal with task-based assessment and its implementation in the Albanian context. In addition, due to insufficient data, these studies fail in providing a well-documented account of the present situation in Albania with regard to Task- based assessment model and its utilization in EFL classrooms. This paper aims to lay out firstly a general overview of this model of learning, and secondly it explores some attempts of how to situate it within the Albanian context. It’s a long and challenging undertaking, but we (teachers) should move forward and try these new experiences out, however demanding they appear.
Task-based Instruction
Task-based is a kind of instruction in which language learners, performing activities, are engaged in meaningful, goal-oriented communication to solve problems, complete projects, and reach decisions. Tasks have been used for a broad range of instructional purposes, serving, for example, as units of syllabuses, activities for structure or function practice, and language focusing enhancements to content-based curricula. In this literature, some issues related to task-based instruction will be discussed.
APPLICATION OF THE FINITE ELEMENT METHOD TO ROTARY-WING AEROELASTICITY.
Recent research in rotary-wing aeroelasticity has indicated that all fundamental problems in this area are inherently nonlinear. The non-linearities in this problem are due to the inclusion of finite slopes, due to moderate deflections, in the structural, inertia and aerodynamic operators associated with this aeroelastic problem. In this paper the equations of motion, which are both time and space dependent, for the aeroelastic problem are first formulated in P.D.E. form. Next the equations are linearized about a suitable equilibrium position. The spatial dependence in these equations is discretized using a local Galerkin method of weighted residuals resulting in a finite element formulation of the aeroelastic problem. As an illustration the method is applied to the coupled flap-lag problem of a helicopter rotor blade in hover. Comparison of the solutions with previously published solutions establishes the convergence properties of the method. It is concluded that this formulation is a practical tool for solving rotary-wing aeroelastic stability or response problems.