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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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.

Longitudinal and lateral-directional dynamic stability. Calculatipon of stall and maximum speeds. Thrust and power diagram calculation. Steady turning performance calculation.

International Standard Atmosphere, measurement of pressure at body surface. Evaluation fulfils the University requirements. Take-off and landibg performance calculation. Lateral-directional control of airplane. Qualitative and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use of an aircraft.

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A3M14AML – Aerodynamics and mechanics of flight – B181

Continuous supersonic expansion, shock waves, aerodynamic heating at supersonic speeds. Steady climbing and gliding flight. Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations. This basic knowledge is required to understand possibilities and limitation of aircraft flights.

Index of /AK_Slany/svazarm/Aerodynamika_a_mechanika_letu/

Take-off and landing performance. Measurement of pressure distribution at airfoil surface. Supersonic flow, supersonic continuous expansion, shock waves. Continuity equation, Bernoulli equation, speed measurement.

Flight with asymmetric thrust. Finite span wing, induced drag, high lift devices, spoilers, vortex generators. Aerodynamic forces and moments.

Mecbanika in horizontal flight, performance at climbing and gliding, performance at turning flight are included. Students will gain information on fluid flows. Assesment methods and criteria linked to learning outcomes. The basics of common mechanics — force effect on a body, kinematics, dynamics. The aerodnyamika offers for students the knowledge necessary for an dynamic stability modes estimation and their influence on aircraft handling, longitudinal and lateral-directional stability.

Subsonic flow around airfoils and wings.

Conditions to obtain the course-unit credit: Learning outcomes of the course unit. 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.

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Transonic range, area rule, supercritical airfoils. Control-fixed neutral point and manoeuvre point of airplane calculation. Supersonic shock-induced drag, aerodynamic heating.

Familiarizing lrtu with the method of assessment of classical theory of performance and a judgment aerpdynamika aerodynamic and propulsion characteristics efficiency on flight performance.

The absence in justifiable cases can be compensated by personal consultation with the lecturer and elaboration of individually assigned topics and exercises.

A3M14AML – Aerodynamics and mechanics of flight – B Forums

Performance requirements of JAR standards. Familiarizing students with the methods of calculation of the stability and aircraft control. Determination of the basic technical aircraft data in the classic aircraft performance and stability and control. Planned learning activities and teaching methods. Compressibility effects, area rule, supercritical airfoils. Supersonic flows, continuous expansion, shock waves.

Mechznika optional programme components.

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