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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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A3M14AML – Aerodynamics and mechanics of flight – B Forums

Supersonic flow, supersonic continuous expansion, shock waves. Assesment methods and criteria linked to learning outcomes. Continuous supersonic expansion, shock waves, aerodynamic heating at supersonic speeds. Specification of controlled education, way of implementation and compensation for absences. Lateral-directional control of airplane.

Flight Mechanics

mechajika Compressibility effects, area rule, supercritical airfoils. Recommended optional programme components. Finite span wing, induced drag, high lift devices, spoilers, vortex generators. Qualitative and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use of an aircraft. Supersonic flows, continuous expansion, shock waves. The course offers for students the knowledge necessary for an dynamic stability modes estimation and their areodynamika on aircraft handling, longitudinal and lateral-directional stability.


Longitudinal and lateral-directional static stability.

Index of /AK_Slany/svazarm/Aerodynamika_a_mechanika_letu/

Conservation laws, stream lines, equations of continuity and Bernoulli, speed measurement, aerodynamic forces. Thrust and power diagram calculation. 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 aerodynamija equations of motion, aircraft state equations.

The absence in justifiable cases can be compensated by personal consultation with the lecturer and elaboration of individually assigned topics and exercises. Performance requirements of JAR standards. Continuity equation, Bernoulli equation, speed measurement. Steady aerldynamika and gliding flight. The exam has written the essential one and oral parts.

Determination of the basic technical aircraft data in the classic aircraft performance and stability and control. International Standard Atmosphere, measurement of pressure at body surface. Calculatipon of stall and maximum speeds. This basic knowledge is required to understand possibilities and limitation of aircraft flights.

Conservation laws, aerodynamic forces aerodynmaika moments ISA. Type of course unit.

Supersonic shock-induced drag, aerodynamic heating. The goal is to explain the basic flight mechanics of atmospheric aircraft. Familiarizing students with the methods of calculation of the stability and aircraft control.

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. Flight mechanics is a follow up to the first part of the course.


Aerodynamics and Flight Mechanics

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

Control-fixed neutral point and manoeuvre point of airplane calculation. The basics of mathematics – differential and integral calculus, common differential equations. The basics of thermomechanics, 1st and 2nd Laws.

Longitudinal and lateral-directional dynamic stability. Transonic leti, area rule, supercritical airfoils.

The basics of common mechanics — force effect on a body, kinematics, dynamics. Take-off and landibg performance calculation. Steady turning performance calculation. Airfoils, wing of finite span. Take-off and landing performance. Conditions to obtain the course-unit credit: Planned learning activities and teaching methods.

Evaluation fulfils the University requirements. Boundary layers, airfoils, polar curve, influence of Reynolds number. Boundary layers, origin of lift, airfoils, finite aerodynamija wings, induced drag, high lif devices. Measurement of pressure distribution at airfoil eltu. Aerodynamic forces and moments. Subsonic flow around airfoils and wings.