Objectives:
Development and application of laser optical measurement techniques for the aerothermodynamic investigation of aero engine components
Applications:
statonary and periodically instationary reacting and non reacting flows in:
axial and centrifugal compressors, axial and radial turbines (rotor and stator), cascades, flames, combustion chambers, nozzles, tubeflows, windtunnels and in-flight applications
Qualifications:
Engineers and physicists with special knowledge in:
optics, electronics, spectroscopy, lasers, particle generation and sizing, light guide fibers, experimental thermodynamics, photodetectors, CCD-cameras, data processing, process control, digital image processing etc.