Schmidt, S.J.; Mihatsch, M.A.; Thalhamer, M.; Adams, N.A. Assessment of Erosion Sensitive Areas via Compressible Simulation of Unsteady Caviating Flows Advanced Experimental and Numerical Techniques of Caviation Erosion PredictionFluid Mechanics and Its ApplicationsSpringer Verl.2014
Örley, F.; Pasquariello, V.; Hickel, S.; Adams, N.A. Cut-element based immersed boundary method for moving geometries in compressible liquid flows with cavitationJournal of Computational Phhysics 2014283pp. 1-22
Kölzsch, A.; Breitsamter, C. Delta Wing Flow Control for the Stall and Post-Stall-Regimepp. 1-10Deutscher Luft- und Raumfahrtkongress [DGLRK2014-0126]2014
Stuhlpfarrer, M.; Breitsamter, C. Numerical and Experimental Investigations of an Electrically Powered Ultralight Aircraftpp. 1-9Deutscher Luft- und Raumfahrtkongress [DGLRK2014-0084]2014
Seywald, K: Gommes de Paule, N.; Wildschek, A.; Holzapfel, F.; Breitsamter, C.; Förster, M. Validation of an aeroelastic analysis and simulation tool for the assessment of innovative, highly elastic aircraft configurationspp. 1-10Deutscher Luft- und Raumfahrtkongress [DGLRK2014-0232]2014
Reß, R.; Grawunder, M.; Breitsamter, C. Parasite Drag Reduction of a Twin-Engine Light Weight Helicopter Configurationpp. 1-10Deutscher Luft- und Raumfhartkongress [DGLRK2014-0046]2014
Hövelmann, A.; Pfnür, S.; Breitsamter, C. Flap Efficiency Analysis for the SAGITTA Diamond Wing Configurationpp. 1-15Deutscher Luft- und Raumfahrtkongress [DGLRK2014-0008]2014
Breitsamter, C.; Grawunder, M.; Reß, R. Aerodynamic Design Optimization for a Helicopter configuration including a Rotating Rotor Headpp. 0686.1-0686.11Congress of the International Council of the Aeronautical Sciences [ICAS-2014-4.9ST]2014
Hövelmann, A.; Breitsamter, C. Experimental Investigation on Vortex Flow Phenomena of a Diamond Wing Configurationpp. 411.1-411.12Congress of the International council of the Aeronautical Sciences [ICAS-2014-4.1.1]2014
Grawunder, M.; Reß, R.; Breitsamter, C. Helicopter Aft Body Drag Reduction by Passive Flow Control pp. 1-12European rotorcraft Forum [ERF-2014-41A]2014