Jobangebot connecticum Job-1769973

DLR-DAAD Doctoral Fellowship Nr. 669: Non-Intrusive Measurement Techniques for Hypersonic Flow Characterization

Deutsches Zentrum für Luft- und Raumfahrt (DLR)

Info zum Arbeitgeber

Deutsches Zentrum für Luft- und Raumfahrt (DLR)

Wissenschaft & Forschung, Luft- und Raumfahrt, Energie, Verkehr, Sicherheit, Digitalisierung

Firmensprache

Deutsch, Englisch

Gründungsjahr

1907

Mitarbeiter

10.001 - 50.000

Branche

Energie, Forschung, IT Hardware, Luft- und Raumfahrttechnik, Sicherheit, Transport und Verkehr

Kontakt

Bei Fragen zu Stellenangeboten aus unserem Jobportal DLR.de/jobs wenden Sie sich bitte an die in den Stellenanzeigen genannten Ansprechpartnerinnen und Ansprechpartner.

Homepage
DLR.de

Karriere-Website
DLR.de/jobs

Doctoral Fellowship
Enter the fascinating world of the German Aerospace Center (Deutsches Zentrum für Luft- und Raumfahrt; DLR) and help shape the future through research and innovation! We offer an exciting and inspiring working environment driven by the expertise and curiosity of our 11,000 employees from 100 nations and our unique infrastructure. Together, we develop sustainable technologies and thus contribute to finding solutions to global challenges. Would you like to join us in addressing this major future challenge? Then this is your place!
Our Institute of Aerodynamics and Flow Technology in Goettingen offers a
DLR-DAAD Doctoral Fellowship
Nr. 669: Non-Intrusive Measurement Techniques for Hypersonic Flow Characterization
What to expect:
The High Enthalpy Shock Tunnel Göttingen (HEG) is a free piston driven shock tunnel commissioned for use in 1991. It is extensively used in a large number of national and international space and hypersonic flight activities and thus is one of the major hypersonic laboratories in Europe. The research activities at HEG are strongly linked to computational fluid dynamics as well as the development of measurement techniques. The scope of the studies covers for instance generic aerodynamic configurations, fundamental aspects of high enthalpy flows, complex hypersonic flight configurations, integrated scramjet configurations and
hypersonic boundary layer transition and transition control strategies.

The technique of Focused Laser Differential Interferometry (FLDI) was successfully applied to hypersonic flows in order to investigate high frequency boundary layer instabilities as well as shock boundary layer interactions in fully turbulent hypersonic flows in HEG. FLDI is an optical technique for the detection of density fluctuations in transparent media. It has gained attention in the hypersonic research community in the recent years, due to its remarkably high bandwidth and its ability to reject highfrequency noise away from the foci. It is therefore a powerful tool to probe the smallest scales of flow field structures, relevant to boundary layer transition and turbulence investigations. The FLDI setup currently operational at HEG is composed of six independent probes, realized by means of a custom-made diffractive optical element. The successful applicant will mechanically and optically advance the existing setup to allow tests in different hypersonic wind tunnels studying the spectral distribution and evolution of free-stream disturbances in a wide range of Mach and Reynolds numbers. The work will result in a unique free-stream disturbance map.

A second focus of the postdoctoral research activity is the Design and realization of a Tunable Diode Laser Absorption Spectroscopy (TDLAS) setup for flow diagnostics in HEG. The activity primarily supports the calibration of the free-stream conditions in HEG by providing additional, independent information on the flow field. TDLAS is an optical measurement technique suitable for use in harsh test environments such as impulse facilities. The technique uses a narrow-line width
monochromatic diode laser as light source which is tuned over the characteristic absorption lines of the target species. Apart from species
concentration the technique can be used to determine gas temperature, pressure and velocity.
What we expect from you:
  • PhD in Aerospace Engineering, Physics or related fields
  • background in experimental hypersonic testing, experience in applied optics
  • English competence: See requirements on www.daad.de/dlr
What we offer:
DLR stands for diversity, appreciation and equality for all people. We promote independent work and the individual development of our employees both personally and professionally. To this end, we offer numerous training and development opportunities. Equal opportunities are of particular importance to us, which is why we want to increase the proportion of women in science and management in particular. Applicants with severe disabilities will be given preference if they are qualified.
Further information:
Starting date: 15.01.2025
Application Deadline: 31.10.2024
Type of employment: Full-time
Contakt:
Dr. Alexander Wagner
Alexander.Wagner@dlr.de

Info zum Arbeitgeber

Deutsches Zentrum für Luft- und Raumfahrt (DLR)

Wissenschaft & Forschung, Luft- und Raumfahrt, Energie, Verkehr, Sicherheit, Digitalisierung

Firmensprache

Deutsch, Englisch

Gründungsjahr

1907

Mitarbeiter

10.001 - 50.000

Branche

Energie, Forschung, IT Hardware, Luft- und Raumfahrttechnik, Sicherheit, Transport und Verkehr

Kontakt

Bei Fragen zu Stellenangeboten aus unserem Jobportal DLR.de/jobs wenden Sie sich bitte an die in den Stellenanzeigen genannten Ansprechpartnerinnen und Ansprechpartner.

Homepage
DLR.de

Karriere-Website
DLR.de/jobs

Info zur Bewerbung
Jobtitel:

DLR-DAAD Doctoral Fellowship Nr. 669: Non-Intrusive Measurement Techniques for Hypersonic Flow Characterization

Jobkennzeichen:
connecticum Job-1769973
Bereiche:
Luft- und Raumfahrttechnik, Physik
Ingenieurwissenschaften: Luft- und Raumfahrttechnik
Naturwissenschaften: Physik
Einsatzort: 37 Göttingen; Niedersachsen
Jobdetails Bewerbungsformular

Jobbörse Job beanstanden