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FSI-OA1Acad. year: 2011/2012
Fundamentals of fluid mechanics – Atmosphere and its properties, fluid properties, fundamental laws of fluid mechanics (recapitulate) – kinematics, dynamics of flow field, viscous effects (state equation, conservation of mass – eq. of continuity, Bernoulli’s eq., Euler’s eq., Navier-Stokes eq.). Airfoil and its aerodynamic properties – origination of aerodynamic forces – physical principle, aerodynamic forces acting on body in moving fluid and their mathematical model, force and moments coefficients, similarity numbers,  - theorem, aircraft wing section. Wing and its aerodynamic properties – wing section – development of airfoils, their marking and classification, structural, operational and technology requirements. High-lift devices. Lift distribution along wingspan, induced drag, total lift, drag and moments of finite span wing. Aerodynamic properties of aircraft – Stability requirements, aerodynamic forces equilibrium. Wing-body combination effects, lift, drag and moment of aircraft, drag polar in detail. Propulsion and its influence. Aerodynamic design and analysis of aircraft.
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branch M-STL , 1 year of study, winter semester, compulsory
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