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Calculatipon of stall and maximum speeds. Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules mechsnika Studies and Examinations.
Take-off and landing performance.
Course detail – Aerodynamics and Flight Mechanics () – BUT
Individual tasks must be finished and handed in the week credits are awarded as the latest. Limitations of turning flight. Familiarizing students x the method of assessment of classical theory of performance and a judgment of aerodynamic and propulsion characteristics efficiency on flight performance. Supersonic shock-induced drag, aerodynamic heating.
Take-off and landibg performance calculation. Students will gain information on fluid flows.
Conservation laws, stream lines, equations of continuity and Bernoulli, speed measurement, aerodynamic forces. The goal aerodynamuka aerodynamic part is concentrated to give students basic knowledge to flow around an aircraft on the base of conservation laws of mass, lrtu and energy.
Continuous supersonic expansion, shock waves, aerodynamic heating at supersonic speeds. The basics of common mechanics — force effect on a body, kinematics, dynamics.
Flight with asymmetric thrust. Assesment methods and criteria linked to learning outcomes. 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 static stability.
Control-fixed neutral point and manoeuvre point of airplane calculation. Students will gain basic information and overview to flows around aircraft. Lateral-directional control of airplane.
Further they will have a clear aerpdynamika of range and endurance, take-off and landing 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.
Planned learning activities and teaching methods. Qualitative and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use of an aircraft.
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. Aerodynamic forces and moments. Measurement of pressure distribution at airfoil surface. Evaluation fulfils the University requirements.
Students will be made familiar with the classical theory of the atmospheric aircraft performance. Conservation laws, aerodynamic forces and moments ISA. Supersonic flow, supersonic continuous expansion, shock waves.
The basics of thermomechanics, 1st and 2nd Laws. Recommended or required reading. Finite span wing, induced drag, high lift devices, spoilers, vortex generators. Type of course unit. Steady turning performance calculation.
Airfoils, wing of finite span. The goal is to explain the basic flight mechanics of atmospheric aircraft.
A3M14AML – Aerodynamics and mechanics of flight – B181
Conditions to obtain the course-unit credit: Performance in horizontal flight, performance at climbing and gliding, performance at turning flight are included. Compressibility effects, area rule, supercritical airfoils.
Steady climbing and gliding flight. Transonic range, area rule, supercritical airfoils.