| Detailed design of a high speed switched reluctance starter/generator for more/all electric aircraft S Shoujun, L Weiguo, D Peitsch, U Schaefer Chinese Journal of Aeronautics 23 (2), 216-226, 2010 | 100 | 2010 |
| Validation and development of loss models for small size radial turbines JF Suhrmann, D Peitsch, M Gugau, T Heuer, U Tomm Turbo Expo: Power for Land, Sea, and Air 44021, 1937-1949, 2010 | 95 | 2010 |
| Three dimensional flow field in a highly loaded compressor cascade C Beselt, M Eck, D Peitsch Turbo Expo: Power for Land, Sea, and Air 45639, V02DT44A018, 2014 | 59 | 2014 |
| Transition mechanisms in laminar separated flow under simulated low pressure turbine aerofoil conditions J Dähnert, C Lyko, D Peitsch Journal of turbomachinery 135 (1), 011007, 2013 | 45 | 2013 |
| Vortex reducer in the high-pressure compressor of a gas turbine S Hein, M Stein, D Peitsch US Patent 7,159,402, 2007 | 41 | 2007 |
| Physics of prestall propagating disturbances in axial compressors and their potential as a stall warning indicator M Eck, S Geist, D Peitsch Applied Sciences 7 (3), 285, 2017 | 39 | 2017 |
| On the effect of volute tongue design on radial turbine performance JF Suhrmann, D Peitsch, M Gugau, T Heuer Turbo Expo: Power for Land, Sea, and Air 44748, 891-901, 2012 | 30 | 2012 |
| Experimental investigations of the aerodynamics of highly loaded tandem vanes in a high-speed stator cascade A Heinrich, C Tiedemann, D Peitsch Turbo Expo: Power for Land, Sea, and Air 50787, V02AT39A005, 2017 | 29 | 2017 |
| Numerical investigation of vortex reducer flows in the high pressure compressor of modern aeroengines D Peitsch, M Stein, S Hein, R Niehuis, U Reinmo¨ ller Turbo Expo: Power for Land, Sea, and Air 36088, 1125-1134, 2002 | 28 | 2002 |
| Influence of the clearance size on rotating instability in an axial compressor stator C Beselt, R van Rennings, R Sorge, D Peitsch, F Thiele, K Ehrenfried, ... 10 th European Conference on Turbomachinery Fluid dynamics & Thermodynamics, 2013 | 26 | 2013 |
| Some aspects on wet compression-physical effects and modeling strategies used in engine performance tools M Obermüller, K Schmidt, H Schulte, D Peitsch Deutsche Gesellschaft für Luft-und Raumfahrt-Lilienthal-Oberth eV, 2012 | 24 | 2012 |
| A new linear high speed compressor stator cascade for active flow control investigations C Tiedemann, A Heinrich, D Peitsch 6th AIAA Flow Control Conference, 3251, 2012 | 23 | 2012 |
| An alternative compressor modeling method within gas turbine performance simulations M Bolemant, D Peitsch Deutsche Gesellschaft für Luft-und Raumfahrt-Lilienthal-Oberth eV, 2014 | 21 | 2014 |
| Hot-acoustic-testrig (hat): A unique facility for thermoacoustic research K Knobloch, C Lahiri, L Enghardt, F Bake, D Peitsch Turbo Expo: Power for Land, Sea, and Air 54679, 1023-1032, 2011 | 20 | 2011 |
| A low speed compressor test rig for flutter investigations L Malzacher, S Geist, D Peitsch, H Hennings Turbo Expo: Power for Land, Sea, and Air 49842, V07BT34A027, 2016 | 19 | 2016 |
| A numerical approach to unstalled and stalled flutter phenomena in turbomachinery cascades S Weber, H Benetschik, D Peitsch, HE Gallus Turbo Expo: Power for Land, Sea, and Air 78712, V004T14A018, 1997 | 19 | 1997 |
| Impact of hub clearance on endwall flow in a highly loaded axial compressor stator C Beselt, D Peitsch, R van Rennings, F Thiele Turbo Expo: Power for Land, Sea, and Air 55249, V06CT42A034, 2013 | 18 | 2013 |
| Prestall instability in axial flow compressors M Eck, R Rückert, D Peitsch, M Lehmann Journal of Turbomachinery 142 (7), 071009, 2020 | 17 | 2020 |
| Numerical Solution of the Navier Stokes Equations for Unsteady Unstalled and Stalled Flow in Turbomachinery Cascades with Oscillating Blades S Weber, HE Gallus, D Peitsch Unsteady Aerodynamics and Aeroelasticity of Turbomachines: Proceedings of …, 1998 | 17 | 1998 |
| Numerical investigation of virtual control surfaces for aeroelastic control on compressor blades V Motta, L Malzacher, D Peitsch Journal of Fluids and Structures 81, 617-637, 2018 | 16 | 2018 |
