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Lamperth, M.U.;Beaudet, A.;Jaensch, M.
Disc motors for automotive applications
Hybrid & Eco Friendly Vehicles Conference 2008 (HEVC 2008)
IEE
2008
Moesl, K.; Vollmer, K.; Sattelmayer, T.; Eckstein, J.; Kopecek, H.
Experimental Study on Laser-Induced Ignition of Swirl-Stabilized Kerosene Flames
383-392
Turbo Expo: Power for Land, Sea, and Air
2008
Albunni, M.N.; Rischmuller, V.; Fritzsche, T.; Lohmann, B.
Model-order reduction of moving nonlinear electromagnetic devices
IEEE Transactions on Magnetics
2008
Volume 44, Issue 7, July 2008, Article number 4520270
pp. 1822-1829
Tielkes, Th.; Kaltenbach, H.-J.; Hieke, M.; Deeg, P.; Eisenlauer, M.
Measures to counteract micro-pressure waves radiating from tunnel exits of DB´s new Nuremberg-Ingolstadt high-speed line
Notes on Numerical Fluid Mechanics and Mulitdisciplinary Design
2008
pp. 40.47
Schmidt, S.J.; Sezal, I.H.; Schnerr, G.H.; Thalhamer, M.
Numerical analysis of Shock Dynamics for Detection of Erosion Senitive Aras in complex 3-D Flows
pp. 107-120
WIMRC Caviation Forum
2008
Schmidt, S.J.; Sezal, I.H.; Schnerr, G.H.; Thalhamer, M.
Riemann techniques for the Simulation of Compressible Liquid flows with Phase-Transition at all Mach numbers - Shock and Wave Dynamics in caviating 3-D Micro and Macro Systems
AEAA Aerospace Sciences Meeting and Exhibit
AIAA paper 2008-1238
2008
Schnerr, G.H.; Sezal, I.H.; Schmidt, S.J.
Numerical Investigation of Three-dimensional cloud cavitation with Special Emphasis on Collapse Induced Shock Dynamics
Physics of Fluids
2008
20, Issue 4, 040703
Furman, A.; Breitsamter, C.
Turbulent and unsteady flow characteristics of delta wing vortex systems
Aerospace Science Meeting & Exhibit
2008
Thouault, N.; Gologan, C.; Breitsamter, C.; Seifert, J.; Adams, N.A.
Experimental investigations on generic fan-in-wing configurations
pp. 1-12
International Powered Lift Conference
2008
Thouault, N.; Gologan, C.; Breitsamter, C.; Adams, N.A.
Aerodynamic Investigations on a Generic Fan-in-Wing Configuration
pp. 351.1-351.12
Congress of the International Council of the Aeronautical Sciences [ICAS-2008-3.5.1]
2008
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