Other
Scientific paper
Feb 2005
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2005esasp.563..275e&link_type=abstract
Proceedings of the Fifth European Symposium on Aerothermodynamics for Space Vehicles (ESA SP-563). 8-11 November 2004, Cologne,
Other
Scientific paper
/RESUME In DLR's arc-heated facility L3K a test campaign was performed on a generic flap model. The model was particularly designed to show influence of thermal fluid/structure interaction when exposed to a high enthalpy flow. Intrusive and non-intrusive measurement techniques were applied to measure the surface temperature distribution and temperature development inside the model. A special method was developed for a more comfortable analysis of infrared images. Comparison of the experimental data to the results of coupled numerical simulations of structure and flow field proved the necessity of considering thermal fluid/structure interactions for the flap configuration.
Esser Bernd
Gölhan A.
Schäfer Rudi
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