Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Friedolin Strauss"'
Autor:
John R. Hurst, S. Hamza Abbas, Heba M. Bintalib, Tiago M. Alfaro, Ulrich Baumann, Siobhan O. Burns, Alison Condliffe, Jesper R. Davidsen, Børre Fevang, Andrew R. Gennery, Filomeen Haerynck, Joseph Jacob, Stephen Jolles, Olivia Lamers, Anne Bergeron, Marion Malphettes, Véronique Meignin, Cinzia Milito, Tomas Milota, Martine Pergent, Antje Prasse, Isabella Quinti, Elisabetta Renzoni, Anna Sediva, Daiana Stolz, Bas Smits, Friedolin Strauss, Annick A.J.M. van de Ven, Joris van Montfrans, Klaus Warnatz
Publikováno v:
ERJ Open Research, Vol 7, Iss 4 (2021)
Externí odkaz:
https://doaj.org/article/7084a0aa8f714798a22a64d7160cde09
Publikováno v:
Language Resources and Evaluation. 55:1127-1140
This report presents a corpus of articulations recorded with Schlieren photography, a recording technique to visualize aeroflow dynamics for two purposes. First, as a means to investigate aerodynamic processes during speech production without any obs
Autor:
Friedolin Strauss, Kilian Claramunt, Alessia Simonini, Cristian Dinescu, Christoph Kirchberger, Hendrik Riedmann, Johan Steelant, Jean-Baptiste Gouriet, Sebastian Soller
Publikováno v:
CEAS Space Journal. 14:187-196
Within a Belgian-German GSTP project, an experimental setup was designed, manufactured and tested to provide data on the behaviour of a shear-driven liquid film. The tests were performed on a flat plate in a rectangular duct using ethanol as film coo
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 18:133-155
Publikováno v:
AIAA Propulsion and Energy 2020 Forum.
Cooling experiments are performed by the DLR Institute of Space Propulsion, applying a transpiration cooling system to a scramjet model combustion chamber. Nitrogen and hydrogen coolants are injected through different porous wall samples made of sint
This publication presents results of the ongoing investigation of transpiration cooling of scramjets conducted at the German Aerospace Center (DLR). It summarizes the results on the influence of the shock-boundary layer interaction on the static wall
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4e3cd8b1371bb928dabe88fde52ccfb9
https://elib.dlr.de/139955/
https://elib.dlr.de/139955/
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
Cooling experiments are performed by the DLR Institute of Space Propulsion, applying a transpiration cooling system to a scramjet model combustion chamber. Hydrogen coolant is injected through different porous wall samples made of sintered stainless
Autor:
Dirk Schneider, Michael Oschwald, Stephan General, Friedolin Strauss, Ralf Stark, Eugeni Costa Ruiz
A numerical simulation of a rectangular supersonic nozzle was conducted to predict the acoustic emissions produced by the jet. The numerical results were compared with experimental measurements. The best agreement between the experiment and simulatio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::46eb6a0d732849a0bfa040db2b8fcebb
https://doi.org/10.2514/6.2019-4116
https://doi.org/10.2514/6.2019-4116
Publikováno v:
2018 Joint Propulsion Conference.
Publikováno v:
53rd AIAA/SAE/ASEE Joint Propulsion Conference.
Transpiration cooling systems are a promising approach to handle the high wall temperatures and heat loads generated in supersonic combustion ramjets (scramjets). The German Aerospace Center DLR has conducted experiments to investigate the applicabil