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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The basics of mathematics – differential and integral calculus, common differential equations. Learning outcomes of the course unit. Continuous supersonic expansion, shock waves, aerodynamic heating at supersonic speeds. Performance requirements of JAR standards. Airfoils, wing of finite span. The basics leetu common mechanics — force aeroynamika on a body, kinematics, dynamics.

Continuity equation, Bernoulli equation, speed measurement. Determination of the basic technical aircraft data in the classic aircraft performance and stability and control. Longitudinal and lateral-directional static stability.

Steady climbing and gliding flight. Control-fixed neutral point and manoeuvre point of airplane calculation. Students will be made familiar with the classical theory of the atmospheric aircraft performance.

Index of /AK_Slany/svazarm/Aerodynamika_a_mechanika_letu/

Students will gain basic information and overview to flows around aircraft. Specification of controlled education, way of implementation and compensation for absences.

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Longitudinal and lateral-directional dynamic stability. Assesment methods and criteria linked to learning outcomes. Familiarizing students with the method of assessment of classical theory of performance and a judgment of aerodynamic and propulsion characteristics efficiency on flight performance.

Flight mechanics is a follow up to the first part of the course. Familiarizing students with the methods of calculation of the stability and aircraft control. The exam has written the essential one and oral parts. Take-off and landing performance. Aerodynamic forces and moments. Individual tasks must be finished and handed in the week credits are awarded as the latest.

Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations.

A3M14AML – Aerodynamics and mechanics of flight – B181

Boundary layers, origin of lift, airfoils, finite span wings, induced drag, high lif devices. Performance in horizontal flight, performance at climbing and gliding, performance at turning flight are included. 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. Boundary layers, airfoils, polar curve, influence of Reynolds number. Qualitative and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use mechannika an aircraft.

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Limitations of turning flight. Supersonic flow, supersonic continuous expansion, shock waves. Take-off and landibg performance calculation.

Type of course unit. Subsonic flow around airfoils and wings.

Course detail – Aerodynamics and Flight Mechanics () – BUT

Conservation laws, aerodynamic forces and moments ISA. Planned learning activities and teaching methods. Lateral-directional control of airplane. This basic knowledge is required to understand possibilities and limitation of aircraft flights.

Steady turning performance calculation. International Standard Atmosphere, measurement of pressure at body surface. The absence in aerodymamika 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

The basics of thermomechanics, 1st and 2nd Laws. Recommended optional programme components. Conditions to obtain the course-unit credit: Finite span wing, induced drag, high lift devices, spoilers, vortex generators. Recommended or required reading. Supersonic flows, continuous expansion, shock waves. Compressibility effects, area rule, supercritical airfoils.