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249983417 16W 2SWS VO Application of Fluidmechanic Calculation Methods for Flight Propulsion   Hilfe Logo

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Application of Fluidmechanic Calculation Methods for Flight Propulsion 
249983417
lecture
2
Winter semester 2016/17
Chair of Turbomachinery and Flight Propulsion (Prof. Gümmer)
(Contact information)
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Allocations: 1 
Angaben zur Abhaltung
Components of gas turbines and aeroengines: inlet, compressor, combustor, turbine, and nozzle.
Engine performance.
Mathematical background: vector and tensor analysis.
Mechanics and thermodynamics of fluid flow, mass conservation, continuity equation, momentum equation, energy equation, stress-extension relations, turbulence models.
Turbomachinery: principals of operation and basic terms, absolute and relative coordinates, similarity equations, characteristic values, compressor and turbine maps.
Calculation of meridian layer (S2-layer): stream line curbature and stream line function, radial equilibrium.
Profiling of rotor and stator blades (S1-layers): fluid flow, supersonic and transonic considerations.
no
German

Students should register for this lecture at the institute's office due to scheduling issues.
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course documents
e-learning course (moodle)