You are not logged in (Log in). A3M14AML – Aerodynamics and mechanics of flight – B Home · Courses · A3M14AML – Aerodynamics and mechanics of. Home; /; aerodynamika a mechanika letu pro piloty a techniky pdf zip, found for you zslg. Deprecated: Non-static method JSite::getMenu() should not be called. Komplexní znalost letounu v kombinaci s nejnovějšími výpočtovými metodami nám umožňuje zvýšit rychlost a zlepšit výkony stroje. Mechanika letu & výkony.
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Supersonic flow, supersonic continuous expansion, shock waves.
Control-fixed neutral point and manoeuvre point of airplane calculation. Continuous supersonic expansion, shock waves, aerodynamic heating at supersonic speeds. Subsonic flow around airfoils and wings.
Further they will have a clear idea of range and endurance, take-off and landing operations, classical theory of the stability and control of aircraft, development of general equations of motion for an atmospheric aircraft, classical small perturbation equations of motion, aircraft state equations.
Students will also learn to judge the influence of aircraft design parameters on its flying characteristics. Boundary layers, origin of lift, airfoils, finite span wings, induced drag, high lif devices. Measurement of pressure distribution at airfoil surface. International Standard Atmosphere, measurement of pressure at body surface. Performance requirements of JAR standards.
Performance in horizontal flight, performance at climbing and gliding, performance at turning flight are included. Type of course unit.
Calculatipon of stall and maximum speeds. Finite span wing, induced drag, high lift devices, spoilers, vortex generators. Learning outcomes of the course unit.
Conditions to obtain the course-unit credit: Flight mechanics is a follow up to the first part of the course. Students will be made familiar with the classical theory of the atmospheric aircraft performance.
Thrust and power diagram calculation.
Index of /AK_Slany/svazarm/Aerodynamika_a_mechanika_letu/
The goal of aerodynamic part is concentrated to give students basic knowledge to flow around an aircraft on the base of conservation laws aerodynakika mass, motion and energy. Airfoils, wing of finite span.
Steady turning performance calculation.
Supersonic flows, continuous expansion, shock waves. Recommended or required reading. Conservation laws, aerodynamic forces and moments ISA. Boundary layers, airfoils, polar curve, influence of Reynolds number.
Aerodynamics and Flight Mechanics
Take-off and landibg performance calculation. Recommended optional programme components. The basics of thermomechanics, 1st and 2nd Laws. Limitations of turning flight. Compressibility effects, area rule, supercritical airfoils.
Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations. Familiarizing students with the methods of calculation of the stability and aircraft control.
The basics of common mechanics — force effect on a body, kinematics, dynamics. Students will gain information aerodynamikka fluid flows. The basics of mathematics – differential and integral calculus, common differential equations.