Study of Total Pressure Losses at the Engine Face of a Submerged Inlet with an Ingested Vortex

Author:

Koch Stefan,Rütten Markus,Rein Martin

Publisher

Springer International Publishing

Reference9 articles.

1. Arntz, A., Atinault, O., Destarac, D., Merlen, A.: Exergy-based aircraft aeropropulsive performance assessment: CFD application to boundary layer ingestion. AIAA 2014-2573 (2014)

2. Rein, M., Koch, S.: Experimental study of boundary-layer ingestion into a diverterless S-duct intake. J. Aircr. Tech. Note 53(11) (2015)

3. Koch, S., Rütten, M., Rein, M.: Experimental and numerical investigations on integrated intakes for agile and highly swept aircraft configurations. DGLR Paper-0173, Deutscher Luft- und Raumfahrtkongress, Rostock (2015). (urn:nbn:de:101:1-201510306355)

4. Berens, T., Delot, A.-L., Tormalm, M., Ruiz-Calavera, L.-P., Funes-Sebastian, D.-E., Rein, M., Säterskog, M., Ceresola, N., Zurawski, L., Numerical and experimental investigations on highly integrated subsonic air intakes. AIAA 2014-0722 (2014)

5. Rein, M., Hannemann, M., Gardner, A.D., Koch, S.: Design of a Generic Subsonic S-Duct Intake for Studies on the Effect of Boundary Layer Ingestion. DLR, Germany Aerospace Center, IB-224-2009-A28, Göttingen, Germany (2009)

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