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Course detail – Aerodynamics and Flight Mechanics () – BUT

This basic knowledge is required to understand possibilities and limitation of aircraft flights. Subsonic flow around airfoils and wings. Take-off and landibg performance calculation.

Performance requirements of JAR standards. Steady turning performance calculation. Flight with asymmetric thrust.

Conservation laws, aerodynamic forces and moments ISA. 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. The exam has written the essential one and oral parts.

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Supersonic flow, supersonic continuous expansion, shock waves.

Individual tasks must be finished and handed in the week credits are awarded as the latest. Boundary layers, origin of lift, airfoils, finite span wings, induced drag, high lif devices. Flight mechanics is a follow up to the first part of the aerodynaika. The basics of mathematics – differential and integral calculus, common differential equations.

Longitudinal and lateral-directional static stability.

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

Type of course unit. Continuous supersonic expansion, shock waves, aerodynamic heating at mechhanika speeds. Lateral-directional control of airplane. Aerodynamic forces and moments.

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

Longitudinal and lateral-directional dynamic stability. Continuity equation, Bernoulli equation, speed measurement. International Standard Atmosphere, measurement of pressure at body surface.

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Calculatipon of stall and maximum speeds. Steady climbing letj gliding flight. Measurement of pressure distribution at airfoil surface. Conservation laws, stream lines, equations of continuity and Bernoulli, speed measurement, aerodynamic forces.

Thrust and power diagram calculation. Transonic range, area rule, supercritical airfoils. Students will gain information on fluid flows. Recommended optional programme components. Recommended or required reading.

A3M14AML – Aerodynamics and mechanics of flight – B161

Evaluation fulfils the University requirements. Take-off and landing performance. Teaching methods depend on the type of course unit as specified in the article 7 aerodynamikx BUT Rules for Studies and Examinations.