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. Measurement of pressure distribution at airfoil surface. Take-off and landing performance. Supersonic shock-induced drag, aerodynamic heating.

Students will be made familiar with the classical theory of the atmospheric aircraft performance. Supersonic flows, continuous expansion, shock waves. Mechanjka Standard Atmosphere, measurement of pressure at body surface.

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

Recommended or required reading. Evaluation fulfils the University requirements. The exam has written the essential one and oral parts.

Students will gain basic information and overview to flows around aircraft. The absence in justifiable cases can be compensated by personal consultation with the lecturer and elaboration of individually assigned topics and exercises. Learning outcomes of the course unit. Familiarizing students with the methods of calculation of the stability and aircraft control.

Performance requirements of JAR standards. Subsonic flow around airfoils and wings. Performance in horizontal flight, performance at aerodtnamika and gliding, performance at turning flight are included. Continuous supersonic expansion, shock waves, aerodynamic heating at supersonic speeds.

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Lateral-directional control of airplane. Airfoils, wing of finite span. Longitudinal and lateral-directional dynamic stability. Boundary layers, airfoils, polar curve, influence of Reynolds number.

Supersonic flow, supersonic continuous expansion, shock waves. Steady climbing and gliding flight.

A3M14AML – Aerodynamics and mechanics of flight – B161

Type of course unit. Assesment methods and criteria linked to learning outcomes.

Longitudinal and lateral-directional static stability. Students will gain information on adrodynamika flows. Students will also learn to judge the influence of aircraft design parameters on its flying characteristics.

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Calculatipon of stall and maximum speeds. Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations. Mechahika and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use of an aircraft. Recommended optional programme components. Finite span wing, induced drag, high lift devices, spoilers, vortex generators. Conservation laws, stream lines, equations of continuity and Bernoulli, speed measurement, aerodynamic forces.

Conditions to obtain the course-unit credit: This basic knowledge is required to understand possibilities and limitation of aircraft flights. 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.


The basics of thermomechanics, 1st and 2nd Laws. Steady turning performance calculation. Flight mechanics is a follow up to the first part of the course. Limitations of turning flight. Thrust and power diagram calculation. Transonic range, area rule, supercritical airfoils. 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.

Aerodynamic forces and moments. Determination of the basic technical aircraft data in the classic aircraft performance and stability and control. Boundary layers, origin of lift, airfoils, finite span wings, induced drag, high lif devices.

The goal is to explain the basic flight mechanics of atmospheric aircraft. Familiarizing students with the method of assessment of classical theory of performance and a judgment of aerodynamic and propulsion characteristics efficiency on flight performance.

Conservation laws, aerodynamic forces and moments ISA. 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.