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Flight with asymmetric thrust. Steady turning performance calculation. Students will be made familiar with the classical theory of the atmospheric aircraft performance. Familiarizing students with the methods of calculation of the stability and aircraft control.

This basic knowledge is required to understand possibilities and limitation of aircraft flights. Take-off and landing performance. Take-off and landibg performance calculation. Type of course leth. Supersonic flows, continuous expansion, shock waves.

Familiarizing students with the method of assessment of classical theory of performance and a judgment of aerodynamic and propulsion characteristics efficiency on flight performance. Measurement of pressure distribution at airfoil surface.


Calculatipon of stall and maximum speeds. Performance requirements of JAR standards. Conditions to obtain the course-unit credit: The absence in justifiable cases can be compensated by personal consultation with the lecturer and elaboration of individually assigned topics and exercises.

Conservation laws, aerodynamic forces and moments ISA. Longitudinal and lateral-directional dynamic stability. Lateral-directional control of airplane.

Continuous supersonic expansion, shock waves, aerodynamic heating at supersonic speeds. Supersonic lrtu, supersonic continuous expansion, shock waves. Performance in horizontal flight, performance at climbing and gliding, performance at turning flight are included.

Control-fixed neutral point and manoeuvre point of airplane calculation.

Learning outcomes of the course unit. Transonic range, area rule, supercritical airfoils.

A3M14AML – Aerodynamics and mechanics of flight – B181

Supersonic shock-induced drag, aerodynamic heating. Students will gain information on fluid flows. The exam has written the essential one and oral parts. Recommended or required reading.

Specification of controlled education, way of implementation and compensation for absences. Planned learning activities and teaching methods.

Steady climbing and gliding flight. Recommended optional programme components. Boundary layers, origin of lift, airfoils, finite span wings, induced drag, high lif devices. 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.


Continuity equation, Bernoulli equation, speed measurement. Conservation laws, stream lines, equations of continuity and Bernoulli, speed measurement, aerodynamic forces. Determination of the basic technical aircraft data in the classic aircraft performance and stability and control.

Flight Mechanics

The course offers for students the knowledge necessary for an dynamic stability modes estimation aerodynamikaa their influence on aircraft handling, longitudinal and lateral-directional stability. Longitudinal and lateral-directional static stability. Aerodynamic forces and moments.