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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Planned learning activities and teaching methods. Calculatipon of stall and maximum speeds.

Aerodynamics and Flight Mechanics

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. Specification of controlled education, way of implementation and compensation for absences.

Familiarizing students with the methods of calculation of the stability and aircraft control. Mechznika flow around airfoils and wings. Evaluation fulfils the University requirements.

Control-fixed neutral point and manoeuvre point of airplane calculation. Assesment methods and criteria linked to learning outcomes. Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations.

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Finite span wing, induced drag, high lift devices, spoilers, vortex generators. Measurement of pressure distribution at airfoil surface. Students will also learn to judge the influence of aircraft design parameters on its flying characteristics. Aerodynamic forces and moments. Students will gain information on fluid flows. Students will gain basic information and overview to flows around aircraft.

Further they will have a clear idea of range and endurance, take-off and landing operations, classical theory of the stability and control of mechanija, development of general equations of motion for an atmospheric aircraft, classical mechannika perturbation equations of motion, aircraft state equations. Conditions to obtain the course-unit credit: The course offers for students the knowledge necessary for an dynamic stability modes estimation and their influence on aircraft handling, longitudinal and lateral-directional stability.

Conservation laws, aerodynamic forces and moments ISA. International Standard Atmosphere, measurement of pressure at body surface.

A3M14AML – Aerodynamics and mechanics of flight – B161

Determination of the basic technical aircraft data in the classic aircraft performance and stability and control. Recommended optional programme components. Steady climbing and gliding flight. Performance in horizontal flight, performance at climbing and gliding, performance at turning flight are included. Longitudinal and lateral-directional static stability. The exam has written the essential one and oral parts. Conservation laws, stream lines, equations of continuity and Bernoulli, speed measurement, aerodynamic forces.

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Boundary layers, airfoils, polar curve, influence of Reynolds number. Type of course unit. Performance requirements of JAR standards. Compressibility effects, area rule, supercritical airfoils.

Thrust and power diagram calculation. Individual tasks must be finished and handed in the week credits are awarded as the latest.

Flight Mechanics

The basics of thermomechanics, 1st and 2nd Laws. Learning outcomes of the course unit. The basics of mathematics – differential and integral calculus, common differential equations. Supersonic flows, continuous expansion, shock waves. Supersonic shock-induced drag, aerodynamic heating. Longitudinal and lateral-directional dynamic stability.

Qualitative and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use of an aircraft. Continuity equation, Bernoulli equation, speed measurement. Transonic range, area rule, supercritical airfoils. Lateral-directional control of airplane. Flight with asymmetric thrust. Supersonic flow, supersonic continuous aerodynamia, shock waves. Take-off and landibg performance calculation. This basic knowledge is required to understand possibilities and limitation of aircraft flights.

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