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

Familiarizing students with the methods of calculation of the stability and aircraft control. Supersonic flow, supersonic continuous expansion, shock waves.

Assesment methods and criteria linked to learning outcomes. Lateral-directional control of airplane.

Flight Mechanics

Students will be made familiar meechanika the classical theory of the atmospheric aircraft performance. Take-off and landibg performance calculation. Transonic range, area rule, supercritical airfoils. The goal is to explain the basic flight mechanics of atmospheric aircraft. Conditions to obtain the course-unit credit: Flight with asymmetric thrust.

Limitations of turning flight. The basics of mathematics – differential and integral calculus, common differential equations.


A3M14AML – Aerodynamics and mechanics of flight – B181

Calculatipon of stall and maximum speeds. Aerodynaika they will have a clear idea of range and endurance, take-off and landing operations, classical theory of the stability and control of mechankia, development of general equations of motion for an atmospheric aircraft, classical small perturbation equations of motion, aircraft state equations.

The exam has written the essential one and oral parts. 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. 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.

Course detail – Aerodynamics and Flight Mechanics () – BUT

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

Supersonic shock-induced drag, aerodynamic heating. Steady climbing and gliding flight. Performance requirements of JAR standards.

Continuity equation, Bernoulli equation, speed measurement. Determination of the basic technical aircraft data in the classic aircraft performance and stability and 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.

Subsonic flow around airfoils and wings. Evaluation fulfils the University requirements. Longitudinal and lateral-directional dynamic stability.

Flight mechanics is a follow up to the first part of the course. Boundary layers, origin of lift, airfoils, finite span wings, induced drag, high lif mechanikw. Longitudinal and lateral-directional static stability. Control-fixed neutral point and manoeuvre point of airplane calculation.

The absence in justifiable cases can be compensated by personal consultation with aerodynamoka lecturer and elaboration of individually assigned topics and exercises. Boundary layers, airfoils, polar curve, influence of Reynolds number. International Standard Atmosphere, measurement of pressure at body surface. Aerodynamic forces and moments. Qualitative and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use of an aircraft.