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Dieter Peitsch
Dieter Peitsch
在 tu-berlin.de 的电子邮件经过验证
标题
引用次数
引用次数
年份
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
1032010
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
962010
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
622014
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
542013
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
442017
Vortex reducer in the high-pressure compressor of a gas turbine
S Hein, M Stein, D Peitsch
US Patent 7,159,402, 2007
412007
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
342002
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
332012
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
322017
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
282013
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
252012
An alternative compressor modeling method within gas turbine performance simulations
M Bolemant, D Peitsch
Deutsche Gesellschaft für Luft-und Raumfahrt-Lilienthal-Oberth eV, 2014
242014
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
242012
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
212011
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
192016
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
191997
Prestall instability in axial flow compressors
M Eck, R Rückert, D Peitsch, M Lehmann
Journal of Turbomachinery 142 (7), 071009, 2020
182020
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
182013
Potentials for pressure gain combustion in advanced gas turbine cycles
N Neumann, D Peitsch
Applied Sciences 9 (16), 3211, 2019
162019
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
162018
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