Modules

6 results

Master's Modules6

Aerodynamik des Flugzeugs 1Fluid-/AerodynamicsIn this module you will learn the fundamentals of calculating and analyzing the aerodynamic forces on aircraft under subsonic conditions. You will acquire knowledge of theoretical models (e.g., potential theory, wing and airfoil theory), airfoil design, and experimental methods, so that you can calculate and evaluate aerodynamic characteristics for airfoils and wings.5 ECTSruns this semesterMW0007AeroelastikFluid-/AerodynamicsYou will learn the basic aeroelastic phenomena that arise from the interaction of elastic, aerodynamic and inertial forces on structures — with a focus on aircraft that are flying with fixed wings. In the end you can derive simple models for static and dynamic aeroelasticity and make quantitative statements about phenomena such as divergence and flutter, as well as assess their limits.5 ECTSruns this semesterMW2228Angewandte CFDFluid-/AerodynamicsYou receive a practice-oriented introduction to numerical fluid dynamics (CFD). You will learn modeling of turbulent flows, numerical methods for solving the Navier–Stokes equations, boundary conditions, grid generation, as well as visualization and evaluation of simulation results and you will apply this practically with ANSYS CFX/ICEM.5 ECTSruns this semesterMW1628GrenzschichttheorieFluid-/AerodynamicsYou deepen the theory of boundary layers based on the Navier–Stokes equations. You learn derivations, analytical solutions and models for incompressible, compressible, two-dimensional and three-dimensional boundary layers as well as temperature boundary layers, stability and turbulence and experimental methods. In the end you can estimate boundary layer problems, derive approximate solutions and describe the transition to turbulence.5 ECTSruns this semesterMW0798GasdynamikFluid-/AerodynamicsYou will learn the fundamentals of compressible flow theory: from the compressible Navier–Stokes equations and thermodynamic principles through stationary flow line theory and shock relations to linear and nonlinear wave dynamics. In the end you will be able to treat stationary and unsteady gas-dynamic problems in sub- and supersonic regimes with analytical methods and to estimate simple multidimensional effects in supersonic flows.5 ECTSno date this semesterMW0357
1 more in Master's ModulesTurbulente StrömungenFluid-/AerodynamicsIn this module you will learn the physical fundamentals and typical phenomena of turbulent flows as well as methods for their statistical description. You will learn how to formulate real flow problems with the basic equations, when turbulence modeling is necessary, and how to select appropriate models (including LES) to investigate flows numerically in an efficient and sufficiently accurate way.5 ECTSno date this semesterMW0595
2 more modules match, but they are taught in German. Show themAeroakustikFluid-/AerodynamicsDu lernst die physikalischen Grundlagen der Aeroakustik: Schallentstehung durch Strömungen, Eigenschaften und quantitative Beschreibung von Schall sowie Ausbreitung und Strahlung in verschiedenen Geometrien. Am Ende kannst du Strömungslärm einordnen, geeignete Prognosemethoden auswählen und Maßnahmen zur Reduzierung oder Eindämmung von Strömungslärm entwerfen.5 ECTSruns this semesterMW1692Aerodynamik des Flugzeugs 2Fluid-/AerodynamicsDu vertiefst die Aerodynamik von Flugzeugen jenseits der Profiltheorie und lernst, wie man endliche Tragflächen, Leitwerke und deren Interaktion sowie transsonische und Überschallphänomene aerodynamisch analysiert. Am Ende kannst du potentialtheoretische Näherungsverfahren anwenden, den Einfluss der Flügelgeometrie auf aerodynamische Derivate bestimmen und aerodynamische Größen für Unterschall-, Transsonic- und Überschallströmungen berechnen.5 ECTSno date this semesterMW0877