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Course detail – Aerodynamics and Flight Mechanics () – BUT

Students will gain information on fluid flows. Individual tasks must be finished and handed in the week credits are awarded as the latest. Lateral-directional control of airplane. Type of course unit. Conditions to obtain the course-unit credit: Measurement of pressure distribution at airfoil surface.

Subsonic flow around airfoils and wings. Aerodynamic forces and moments. Students will gain basic information and overview to flows around aircraft. Recommended or required reading. Steady climbing and gliding flight. The basics of mathematics – differential and integral calculus, common differential equations. 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 perturbation equations of motion, aircraft state equations.

Familiarizing students with the methods of calculation of the stability and aircraft control. Calculatipon of stall and maximum speeds.


Take-off and landibg performance calculation. Students will be made familiar with the classical theory of the atmospheric aircraft performance. Longitudinal and lateral-directional dynamic stability. Planned learning activities and teaching methods. 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.

This basic knowledge is required to understand possibilities and limitation of aircraft flights. Continuous supersonic expansion, shock waves, aerodynamic heating at supersonic speeds. Steady turning performance calculation.

Evaluation fulfils the University requirements. Supersonic flows, continuous expansion, shock waves. Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations. Supersonic flow, supersonic continuous expansion, mecyanika waves. The goal is to aetodynamika the basic flight mechanics of atmospheric aircraft.

Flight mechanics is a follow up to the first part of the course. The basics of thermomechanics, 1st and 2nd Laws.

A3M14AML – Aerodynamics and mechanics of flight – B161

Performance in horizontal flight, performance at climbing and gliding, performance at turning flight are included. Supersonic shock-induced drag, aerodynamic heating. Finite span wing, induced drag, high lift devices, spoilers, vortex generators.

Conservation laws, aerodynamic forces and moments ISA. Performance requirements of JAR standards. Assesment methods and criteria linked to learning outcomes. Students will also learn to judge the influence of aircraft design parameters on its flying characteristics. Flight with asymmetric thrust. Boundary layers, origin of lift, airfoils, finite span wings, induced drag, high lif devices. Take-off and landing performance. Conservation laws, stream lines, equations of continuity and Bernoulli, speed measurement, aerodynamic forces.

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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. Boundary layers, airfoils, polar curve, influence of Reynolds number.

Transonic range, area rule, supercritical airfoils. 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. Familiarizing students with the method of assessment of classical theory of performance and a judgment of aerodynamic and propulsion characteristics efficiency on flight performance. International Standard Atmosphere, measurement of pressure at body surface.

The exam has written the essential one and oral parts. The basics of common mechanics — force effect on a body, kinematics, dynamics. Qualitative and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use of an aircraft.

Longitudinal and lateral-directional static stability. Recommended optional programme components. Compressibility effects, area rule, supercritical airfoils. Learning outcomes of the course unit. Airfoils, wing of finite span. Determination of the basic technical aircraft data in the classic aircraft performance and stability and control.