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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Recommended or required reading. The goal is to explain the basic flight mechanics of atmospheric aircraft.
Aerodynamics and Flight Mechanics
Boundary layers, origin of lift, airfoils, finite span wings, induced drag, high lif devices. Students will also learn to judge the influence of aircraft design parameters on its flying characteristics. Conservation laws, aerodynamic forces and moments ISA. Longitudinal and lateral-directional static stability. Conditions to obtain the course-unit credit: Students will gain information on fluid flows.
Continuity equation, Bernoulli equation, speed measurement. Recommended optional programme components. Limitations of turning flight.
Familiarizing students with the methods of calculation of the stability and aircraft control. Supersonic flow, legu continuous expansion, shock waves. Calculatipon of stall and maximum speeds. Transonic range, area rule, supercritical airfoils. Performance requirements of JAR standards. 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.
Learning outcomes of the course unit. International Standard Atmosphere, mechanikx of pressure at body surface.
A3M14AML – Aerodynamics and mechanics of flight – B Calendar: Upcoming events
Determination of the basic technical aircraft data in the classic aircraft performance and stability and control. The basics of thermomechanics, 1st and 2nd Laws. Type of course unit. Planned learning activities and teaching aerodynamia. Evaluation fulfils the University requirements.
Further they will have a clear idea of aeerodynamika and endurance, take-off and landing operations, classical theory of the aerldynamika and control of aircraft, development of general equations of motion for an atmospheric aircraft, classical small perturbation equations of motion, aircraft state equations.
Compressibility effects, area rule, supercritical airfoils. Students will gain basic information and overview to flows around aircraft. Take-off and landing performance. Individual tasks must be finished and handed in the week credits are awarded as the latest.
Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations.
Control-fixed neutral point and manoeuvre point of airplane calculation. Aeordynamika and landibg performance calculation. Flight mechanics is a follow up to the first part of the course.
Assesment methods and criteria linked to learning outcomes. Steady climbing and gliding flight. Familiarizing students with the method of assessment of classical theory of performance and a judgment of aerodynamic and propulsion characteristics efficiency on flight performance.
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The absence in justifiable cases can be compensated by personal consultation with the lecturer and elaboration of aerodynqmika assigned topics and exercises. Qualitative and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use of an aircraft.
Finite span wing, induced drag, high lift devices, spoilers, vortex generators. Students will be made familiar with the classical theory of the atmospheric aircraft performance. Supersonic shock-induced drag, aerodynamic heating. This basic knowledge is required to understand possibilities and limitation of aircraft flights.
Steady turning performance calculation. Lateral-directional mecchanika of airplane.