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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Boundary layers, origin of lift, airfoils, finite span mechanikq, induced drag, high lif devices. Performance in horizontal flight, performance at climbing and gliding, performance at turning flight are included.

Conservation laws, aerodynamic forces aeroddynamika moments ISA. Supersonic shock-induced drag, aerodynamic heating. Flight mechanics is a follow up to the first part of the course.

Aerodynamics and Flight Mechanics

The goal mrchanika 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. Aerodynamlka range, area rule, supercritical airfoils. Qualitative and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use of an aircraft.

Type of course unit. 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. International Standard Atmosphere, measurement of pressure at body surface.


A3M14AML – Aerodynamics and mechanics of flight – B Forums

Learning outcomes of the course unit. Flight with asymmetric thrust.

Assesment methods and criteria linked to learning petu. Supersonic flows, continuous expansion, shock waves. Finite span wing, induced drag, high lift devices, spoilers, vortex generators.

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

Airfoils, wing of finite span. Continuity equation, Bernoulli equation, speed measurement. Calculatipon of stall and maximum speeds. Continuous supersonic expansion, shock waves, aerodynamic heating at supersonic speeds.

Steady climbing and gliding flight. Conditions to obtain the course-unit credit: The basics of common mechanics — petu effect on a body, kinematics, dynamics. Students will gain information on fluid flows.

Students will also learn to judge the influence of aircraft design parameters on its flying characteristics. Longitudinal and lateral-directional static stability. Determination of the basic technical aircraft data in the classic aircraft performance and stability and control.

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. Supersonic flow, supersonic continuous expansion, shock waves. The exam has written the essential one and oral parts. Performance requirements of JAR standards.

The goal is to explain the basic flight aerodyhamika of atmospheric aircraft. Measurement of pressure distribution at airfoil surface. Conservation laws, stream lines, equations of continuity and Bernoulli, speed measurement, aerodynamic forces. Subsonic flow around airfoils and wings. Limitations of turning flight. Lateral-directional control of airplane.


The absence in justifiable cases can be compensated by personal consultation with the lecturer and elaboration of individually assigned topics and exercises. Compressibility effects, area rule, supercritical airfoils.

Take-off and landing performance. Specification of controlled education, way of implementation and compensation for absences. Students will gain basic information and overview to flows around aircraft. Boundary layers, airfoils, polar curve, influence of Reynolds number.

The basics of thermomechanics, 1st aefodynamika 2nd Laws. Recommended or required reading. Longitudinal and lateral-directional dynamic stability. 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 mathematics – differential and integral calculus, common differential equations.

Familiarizing students with the methods of calculation of the stability and aircraft control.

Recommended optional programme components. Take-off and landibg performance calculation. Planned learning activities and teaching methods.