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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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. Take-off and landibg performance calculation. Familiarizing students with the method of assessment of classical theory of performance and a judgment of aerodynamic and propulsion characteristics efficiency on flight performance. International Standard Atmosphere, measurement of pressure at body surface. Planned learning activities and teaching methods.

Further they will have a clear idea of range and endurance, take-off and landing operations, classical theory of the stability arrodynamika control of aircraft, development of general equations of motion for an atmospheric aircraft, classical small perturbation equations of motion, aircraft state equations.

Aerodynamic forces and moments. Thrust and power diagram calculation. Lateral-directional control of airplane.

Aerodynamics and Flight Mechanics

Students will be made familiar with the classical theory of the atmospheric aircraft performance. Flight with asymmetric thrust. Finite span wing, induced drag, high lift devices, spoilers, vortex generators. The exam has written the essential one and oral parts. Longitudinal and lateral-directional dynamic stability. Continuous supersonic expansion, shock waves, aerodynamic heating at supersonic speeds.


Index of /AK_Slany/svazarm/Aerodynamika_a_mechanika_letu/

Specification of controlled education, way of implementation and compensation for absences. Supersonic shock-induced drag, aerodynamic heating. Compressibility effects, area rule, supercritical airfoils. Familiarizing students with the methods of calculation of the stability and aircraft control.

Assesment methods and criteria linked to learning outcomes. Airfoils, wing of finite span.

A3M14AML – Aerodynamics and mechanics of flight – B Calendar: Upcoming events

Continuity equation, Bernoulli equation, speed measurement. Flight mechanics is a follow up to the first part of the course. Conservation laws, aerodynamic forces and moments ISA. Steady turning performance calculation.

Take-off and landing performance. Qualitative and quantitative appraisal of aircraft meechanika and stability and control regarding the design and optimal use of an aircraft. Measurement of pressure distribution at airfoil surface.

Students will gain basic information and overview to flows around aircraft. Conservation laws, stream lines, equations of continuity and Bernoulli, speed measurement, aerodynamic forces.

The basics of common mechanics — force effect on a body, kinematics, dynamics.

Type of course unit. Supersonic flow, supersonic continuous expansion, shock waves.

The absence in justifiable cases can be compensated by personal consultation with the lecturer and elaboration of individually assigned topics and exercises. Steady climbing and gliding flight. This basic knowledge is required to understand possibilities and limitation of aircraft flights. Learning outcomes of the course unit. Boundary layers, airfoils, polar curve, influence of Reynolds number.


Control-fixed neutral point and manoeuvre point of airplane calculation. Calculatipon of stall and maximum speeds. Subsonic flow around airfoils and wings.

The basics of mathematics – differential and integral calculus, common differential equations. Students will also learn to judge the influence of aircraft design parameters on its flying characteristics.

Evaluation fulfils the University requirements. Mechaniia will gain information on fluid flows. Limitations of turning flight. Supersonic flows, continuous expansion, shock waves. Boundary layers, origin of lift, airfoils, finite span wings, induced drag, high lif devices.

Transonic range, area rule, supercritical airfoils.

A3M14AML – Aerodynamics and mechanics of flight – B181

Recommended optional programme components. 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. Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations. Longitudinal and lateral-directional static stability.