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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Take-off and landibg performance calculation. The basics of thermomechanics, 1st and 2nd Laws. Aerodynamic forces and moments. Lateral-directional control of airplane. Qualitative and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use of an aircraft.
Transonic range, area rule, supercritical airfoils. Take-off and landing performance. Supersonic flow, supersonic continuous expansion, shock waves.
A3M14AML – Aerodynamics and mechanics of flight – B161
Supersonic flows, continuous expansion, shock waves. Further they will have a clear idea of range and endurance, take-off and aerodnamika 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.
Recommended or required reading. Control-fixed neutral point and manoeuvre point of airplane calculation. Evaluation fulfils the University requirements.
Specification of controlled education, way of implementation and compensation for absences. Longitudinal and lateral-directional static stability. Finite span wing, induced drag, high lift devices, spoilers, vortex generators. Type of course unit. Students will gain information on fluid flows. Steady turning performance calculation. Performance in horizontal flight, performance at climbing and gliding, performance at turning flight are included.
Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations. Conditions to obtain the course-unit credit: Boundary layers, origin of lift, airfoils, finite span wings, induced drag, high lif devices.
The basics of mathematics – differential and mehcanika calculus, common differential equations. Determination of the basic technical aircraft data in the classic aircraft performance and stability and control. Compressibility effects, area rule, supercritical airfoils. Supersonic shock-induced drag, aerodynamic heating. Individual tasks must be finished and handed in the week credits are awarded as the latest.
Measurement of pressure distribution at airfoil surface. The basics of common mechanics — force effect on a body, kinematics, dynamics. Students will gain basic information and overview to flows around aircraft. Continuous supersonic expansion, shock waves, aerodynamic heating at supersonic speeds.
Conservation laws, stream lines, equations of continuity and Bernoulli, speed measurement, aerodynamic forces. The absence in justifiable cases aerkdynamika be compensated by personal consultation with the lecturer and elaboration of individually assigned topics and exercises. Thrust and power diagram calculation. Airfoils, wing of finite span. Performance requirements of JAR standards.
Students will also learn to judge the influence of aircraft design parameters on its flying characteristics. Longitudinal and lateral-directional dynamic stability. Conservation laws, aerodynamic forces and moments ISA. Recommended optional programme components. The exam has written the essential one and oral parts. 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.
Learning outcomes of the course unit. Familiarizing students with the method of assessment of classical theory of performance and a judgment of aerodynamic and propulsion characteristics efficiency on flight performance. The goal of aerodynamic part is concentrated to give students basic knowledge to flow around an aircraft on the base of conservation xerodynamika of mass, motion and energy.