AERODYNAMIKA A MECHANIKA LETU PDF

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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Students will gain information on fluid flows.

This basic knowledge is required to understand possibilities and limitation of aircraft flights. The basics of thermomechanics, 1st and 2nd Laws.

Performance requirements of JAR standards. Control-fixed neutral point and manoeuvre point of airplane calculation. Subsonic flow around airfoils and wings.

Aerodynamika a mechanika letu pro plachtaře – Radoslav Jíra – Google Books

Take-off and landing performance. Flight mechanics is a follow up to the first part of the course. Boundary layers, origin of legu, airfoils, finite span wings, induced drag, high lif devices. Familiarizing students with the method of assessment of classical theory of performance and a judgment of aerodynamic and propulsion characteristics efficiency on flight performance.

Learning outcomes of the course unit.

Aerodynamics and Flight Mechanics

Supersonic flow, supersonic continuous expansion, shock waves. Measurement of pressure distribution at airfoil surface. Students will also learn to judge the influence of aircraft design parameters on its flying characteristics.

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Limitations of turning flight. Conservation laws, stream lines, equations of continuity and Bernoulli, speed measurement, aerodynamic forces. Recommended optional programme components. Recommended or required reading. Determination of the basic technical aircraft data in the classic aircraft performance and stability and control. Familiarizing students with the methods of calculation of the stability and aircraft control. The basics of mathematics – differential and integral calculus, common differential equations.

Finite span wing, induced drag, high lift devices, spoilers, vortex generators. Continuity equation, Bernoulli equation, speed measurement. Steady turning performance calculation.

Steady climbing and gliding flight. The exam has written the essential one and oral parts. Airfoils, wing of finite span. Students will gain basic information and overview to flows around aircraft. Flight with asymmetric thrust. Longitudinal and lateral-directional dynamic stability. The basics of common mechanics — force effect on a body, kinematics, dynamics. Students will be made familiar with the classical theory of the atmospheric aircraft performance.

Lateral-directional control of airplane. Aerodynamic forces and moments. Qualitative and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use of an aircraft.

The absence in justifiable cases can be compensated by personal consultation with the lecturer and elaboration of individually assigned topics and exercises. Conditions to obtain the course-unit credit: 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.

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Conservation laws, aerodynamic forces and moments ISA.

Index of /AK_Slany/svazarm/Aerodynamika_a_mechanika_letu/

Supersonic flows, continuous expansion, shock waves. Boundary layers, airfoils, polar curve, influence of Reynolds number. Planned learning activities and teaching methods.

Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations.

Performance in horizontal flight, performance at climbing and gliding, performance at turning flight are included. Calculatipon of stall and maximum speeds.

Type of course unit. The goal of aerodynamic part is concentrated to give students basic knowledge to flow around an aircraft on the base of conservation laws of mass, motion and energy.

International Standard Atmosphere, measurement of pressure at body surface. Specification of controlled education, way of implementation and compensation for absences.

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