. "Aeronautics"@en . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . "Aircraft propulsion"@en . . "no data" . "Anotation:\r\n\r\nThis course gives basic knowledge of the aircraft propulsion theory, thermal cycles of aircraft powerplants and basics of aero- and thermodynamics of aircraft powerplants components. The influence of design parameters on propulsion system efficiency, specific fuel consumption and thrust is analyzed for the given flight velocity. Design layouts of the aerospace propulsion units are introduced and function of their components is described. The focus is given on the comparison of various systems and the choose of the appropriate one. Enviromental aspects are mentioned together with the common and alternative fuels and energy sources.\r\nStudy targets:\r\n\r\nThe goal of study is the description of the enegetical transformation in aerospace propulsion systems and their properties.\r\nCourse outlines:\r\n\r\n1.\t \tHistorical overview, forces acting on an aircraft, thrust, power, efficiency\r\n2.\t \tPropulsion systems, their thrust and power\r\n3.\t \tPropeller, basic aerodynamics, thrust, power, efficiency and dimensionless parameters\r\n4.\t \tApplied thermodynamics and aerodynamics\r\n5.\t \tAircraft piston engines\r\n6.\t \tTurbine engines\r\n7.\t \tBasics of the turbomachinery aerodynamics\r\n8.\t \tAxial and radial compressors\r\n9.\t \tTurbines for aircraft powerplants\r\n10.\t \tIntake ducts and nozzles\r\n11.\t \tCombustion chambers\r\n12.\t \tTurbojet, turbofan and turboprop engines\r\n13.\t \tDependence of powerplant characteristics on the flight velocity and altitute\r\n14.\t \tNoise and enviromental issues of aircraft powerplants\r\nExercises outline:\r\n\r\nExcercises are focused on the practising of computational methods which were explained during lectures. Basic methods are used to determine thrust, power and efficiency for aircraft powerplants and propellers. Advantages and disadvantages of various propulsion systems are analyzed and compared. Results are discussed in order to obtain theoretical background for choosing of the appropriate propulsion system for given aircraft." . . "no data"@en . "TRUE" . . "Master of Aerospace Engineering"@en . . "https://aerospace.fel.cvut.cz/overview" . "120"^^ . "Presential"@en . "This is a Master degree study programme focused on education and training of nowadays and/or future specialists in the field of aeronautical and space systems and technologies. Although the programme is taught at the Faculty of Electrical Engineering, it can be considered as a whole-university program, because of a strong link with the Faculty of Mechanical Engineering where several compulsory courses are given. Even if the program puts the emphasis on aerospace fields, the education is supported by a broad knowledge of electronics, embedded systems and their design, programming and usage. Moreover, the program curriculum is extended by soft skills’ training. The program content is in accordance with prestigious European aerospace universities and thus provides good competitive basis for graduates’ future employment in variety of private and state companies and institutions.\nThe study is hands-on focused. Students can thus develop their practical knowledge via practical oriented courses and individual projects. A full 4th semester of the study is dedicated to a diploma thesis which can also be solved in cooperation with industry and abroad. The CTU and program itself have strong links with European aerospace universities via PEGASUS Network which supports student exchange program and getting experience from other country.\nThe program introduces current state-of-the-art in the field of aerospace but expects graduates to be fluent also in the future technologies and systems."@en . . . "no data"@en . "FALSE" . . . "Master"@en . "Thesis" . "Not informative" . "no data"@en . "Not informative" . "Recommended" . "aircraft and spacecraft engineering, avionics, integrated systems with their subparts in terms of sensors, data processing, buses, communication, and integration, radio systems, flight control, inertial-GNSS-decision based navigation, trajectory planning."@en . "1"^^ . "FALSE" . "Upstream"@en . . . . . . . . . . . . . . . . .