There is much to be said about affecting AND affectability of the poet in the sphere of literary criticism, AND few poets can be accounted for who have benefited only from their own hearts' proclamation AND have not been affected by their previous literary traditions. Looking at the poets' diwans with this horizon of view can reveal the limits of innovation, literary style, methods AND traditions of poetry AND the way to attain the perfection of theme AND provide the process of understANDing the poets' works.This essay deals with the affectability of Safi Alishah from the previous poets to illuminate the horizons of his thought more explicitly.

What in Hermeneutics AND the domain of political thought is considered as the main question: "what approach should be adopted for understANDing the meaning of a text or essay?" To answer this question, textualism AND theme tendency for reviewing AND interpretation of thoughts AND ideas have been formed. A third approach in reaction to those two approaches has been materialized with emphasis on linguistic topics AND author's aim AND intention. This third approach in the domain of political thought is mostly shown in the beliefs of the political thought historian, Quentin Skinner. Skinner is the professor of political science in Cambridge University. In his opinion, the text is a realization of an intentional communicative act in a particular ideological-historical AND intellectual atmosphere. Each sentence contains a particular intention about a particular case or opportunity aimed at solving a particular problem. Within the domain of thought AND philosophy, there are no permanent AND common questions or problems AND no permanent AND meta-time answers. He is of the belief that in order to understAND the meaning of the text which is the objective visualization of writer's intention AND aim, it is essential to comprehend his/her thoughts. This purpose of course is not solely mental but is also a social act which finds objectivity in the time of author's language. In order to comprehend the aim AND intention of an author, in addition to the language AND concepts of his time, it is also necessary to know the social, historical AND intellectual background AND foundations of his/her era.

In this paper, two-dimensional AND axisymmetric, time dependent transonic AND supersonic flows over a projectile overtaking a moving shock wave are considered. The flow is simulated numerically by solving full time averaged Navier-Stokes equations. The equations are linearized by Newton approach. The Roe's flux splitting method, second order central difference scheme for the diffusion terms AND the second order approximation for time derivatives are used. For the turbulence terms, the Baldwin-Lomax AND mixing length turbulence models are used. The present algorithm captures complicated features of flow including moving shock waves, expansion waves, boundary layers AND wakes AND their interactions. The results show that as the projectile passes through the moving shock wave, it changes the flow field features AND pressure distribution dramatically. The drag force decreases AND even becomes negative while the projectile takes over the shock wave. The flow features AND the aerodynamic forces in transonic flow changes much more than those in the supersonic flow as the projectile passes through the shock wave. The results show that when the shock wave passes though the projectile, the flow field structures AND the aerodynamic forces change abruptly. The drag force reduces AND the shock wave passes through the projectile. Such variations are more vociferous for transonic flows than the supersonic flows. For transonic flows, the drag force changes sign AND accelerates the projectile. Such behavior is important when the stability AND control of the projectile are studied. Also such changes in pressure around the projectile AND in the wake region change the projectile projectory.