. "Aeronautics"@en . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . "Modeling, simulation and application of propulsion and power systems"@en . . "5.00" . "Course Contents 2nd EDUCATION PERIOD\nPart 1 (2 ECTS)\nModule 1 Introduction, Context, Foundations\nModule 2 Conservation equations\nModule 3 Modeling paradigms\nModule 4 Numerical methods and software\nModule 5 Modelica\nModule 6 Constitutive equations\nModule 7 Components and system modeling\nModule 8 Verification and validation\n3rd EDUCATION PERIOD\nPart 1 (1 ECTS)\nModule 9 Model-based control\nTake Home exam\nPart 2 (2 ECTS)\nModule 10 - Team Project to be chosen among\na Aero engine with GSP or GTPsim\nb Power or propulsion system with Modelica\nStudy Goals After learning the content of the course, the student will be able to:\nGiven an engineering problem related to propulsion and power systems, use the 9-steps method to create or select the appropriate\nmodel and run and interpret simulations in order to obtain a good solution of such problem, and communicate the results.\nIn particular, this overarching objective can be obtained by developing the following theoretical capabilities:\n1. Describe the role and types of models in Propulsion and Power Systems Engineering, and define which different modeling\nparadigms and numerical methods are most appropriate or needed to develop a system model given its purpose.\n2. Formulate a mathematical model for a typical propulsion and power system or component, by first analyzing the functionality\nof a system by means of a process flow diagram; by defining the energy, mass, and momentum conservation balances for the\nsystem of interest, and choosing the most appropriate form of conservation equations; by selecting the constitutive equations\nrequired to close the mathematical model (thermophysical models of fluids, chemical reaction eqs, heat transfer correlations,\netc.).\n3. Choose and configure numerical techniques for the solution of non-linear algebraic and differential-algebraic equation systems,\nwhich result from the formulation of a mathematical model.\n4. Implement and code a system model of a power and propulsion application by adopting an object-oriented modeling approach\n(use of modularity, hierarchy, predefined connectors and inter-module variables).\n5. Evaluate the reliability and possibly the fidelity of a model in the light of its purpose (model validation)\n6. Use system models to solve engineering problems such as system performance assessment, preliminary design of the system\nand its components, the design of control strategies and the tuning of controller parameters, as well as communicate the results of\nthe engineering analysis both verbally, and by means of a technical report." . . "Blended"@en . "TRUE" . . "Master in Aerospace engineering"@en . . "Luchtvaart- en Ruimtevaarttechniek (tudelft.nl)" . "120"^^ . "Presential"@en . "In the MSc programme in Aerospace Engineering, you will have abundant opportunities for working on projects and internships across the globe, taking advantage of established relationships with Schiphol Airport, the European Space Agency, KLM, Airbus and other aerospace industries and research institutes. You will also have the option of working as a team member in international competitions in extra-curricular activities.\n\nAt TU Delft, you will obtain hands-on experience whilst working in test and laboratory facilities that are unsurpassed in Europe. Our facilities include low-speed and high-speed (up to Mach 11) wind tunnels, GPS measurement stations, the Structures and Materials Laboratory, the SIMONA research flight simulator, a Cessna Citation II flying laboratory, a collection of large and small aircraft and spacecraft parts, the Delfi Ground Station for satellite communications and a clean room for research and training on our own university satellites."@en . . . . . . . . . "2"@en . "FALSE" . . "Master"@en . "Thesis" . "2314.00" . "Euro"@en . "20560.00" . "Mandatory" . "no data"@en . "6"^^ . "TRUE" . "Upstream"@en . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .