Volume 3, Issue 1
مرور بر اساس
ارسال های اخیر
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Application of A Simulation Algorithm for Dynamic and Nonlinear Analysis of A Liquid Propellant Engine (Iranian Aerospace Society, 2006-01-01)In this paper application of a simulation algorithm for dynamic and nonlinear analysis of a specific liquid propellant engine is presented. The mathematical model of the engine includes a set of nonlinear algebraic equations ...
 
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Numerical Study of Reynolds Number Effects on Flow over a Wall-Mounted Cube in a Channel Using LES (Iranian Aerospace Society, 2006-01-01)Turbulent flow over wall-mounted cube in a channel was investigated numerically using Large Eddy Simulation. The Selective Structure Function model was used to determine eddy viscosity that appeared in the subgrid scale ...
 
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Nonlinear Optimal Control Techniques Applied to a Launch Vehicle Autopilot (Iranian Aerospace Society, 2006-01-01)This paper presents an application of the nonlinear optimal control techniques to the design of launch vehicle autopilots. The optimal control is given by the solution to the Hamilton-Jacobi-Bellman (HJB) equation, which ...
 
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Selection of Favorite Reusable Launch Vehicle Concepts by using the Method of Pairwise Comparison (Iranian Aerospace Society, 2006-01-01)The contribution of this paper to the space transportation system field is to select promising Reusable Launch Vehicle (RLV) concepts by using a formal evaluation procedure. The vehicle system is divided into design features. ...
 
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Numerical Simulation of Flow Past Oscillating Airfoil Using Oscillation of Flow Boundary Condition (Iranian Aerospace Society, 2006-01-01)The present study is devoted to an approximate modeling for numerical simulation of flows past oscillating airfoils. In this study, it is shown that the harmonic oscillating objects can be studied by simple numerical codes ...
 
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Experimental Study of Vortex Shapes behind a Wing Equipped with Different Winglets (Iranian Aerospace Society, 2006-01-01)An extensive experimental study is conducted to examine effects of different winglet-shapes and orientations on the vortex behind a wing, static surface pressure over the wing, and wing wake of a swept wing at various ...
 



