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 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.

Supersonic shock-induced drag, aerodynamic heating. Transonic range, area rule, supercritical airfoils. Students will also learn to judge the influence of aircraft design parameters on its flying characteristics. Familiarizing students with the methods of calculation of the stability and aircraft control. Conservation laws, aerodynamic forces and moments ISA. The goal is to explain the basic flight mechanics of atmospheric aircraft. Students will gain information on fluid flows.

Thrust and power diagram calculation. This basic knowledge is required to understand possibilities and limitation of aircraft flights. Conservation laws, stream lines, equations of continuity and Bernoulli, speed measurement, aerodynamic forces. Qualitative and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use of an aircraft. Airfoils, wing of finite span.

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Planned learning activities and teaching methods. Conditions to obtain the course-unit credit: Aerodynamic forces and moments. Longitudinal and lateral-directional dynamic stability. International Standard Atmosphere, measurement of pressure at body surface. Boundary layers, origin of lift, airfoils, finite span wings, induced drag, high lif devices.

Learning outcomes of the course unit. 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. The basics of thermomechanics, 1st and 2nd Laws. Control-fixed neutral point and manoeuvre point of airplane calculation. Determination of the basic technical aircraft data in the classic aircraft performance and stability and control.

mchanika

A3M14AML – Aerodynamics and mechanics of flight – B161

Measurement of pressure distribution at airfoil surface. Recommended optional programme components. The basics of common mechanics — force effect on a body, kinematics, dynamics. Performance requirements of JAR standards.

Performance in horizontal flight, performance at climbing and gliding, performance at turning flight are included. Recommended or required reading. Supersonic flow, supersonic continuous expansion, shock waves.

Flight Mechanics

Subsonic flow around airfoils and wings. Compressibility effects, area rule, supercritical airfoils. Finite span wing, induced drag, high lift devices, spoilers, vortex generators. Evaluation fulfils the University requirements. Type of course unit.

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Assesment methods and criteria linked to learning outcomes. Limitations of turning flight.

Index of /AK_Slany/svazarm/Aerodynamika_a_mechanika_letu/

Arrodynamika mechanics is a follow up to the first part of the course. 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. Continuous supersonic expansion, shock waves, aerodynamic heating at supersonic speeds. Longitudinal and lateral-directional static stability. Calculatipon of stall and maximum speeds.

Boundary layers, airfoils, polar curve, influence of Reynolds number. Familiarizing students with the method of assessment of classical theory of performance and a judgment of aerodynamic and propulsion characteristics efficiency on flight performance. Take-off and landibg performance calculation. Specification of controlled education, way of implementation and compensation for absences. Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations.

Individual tasks must be finished and handed in the week credits are awarded as the latest.