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Results: 1-9 |
Results: 9
Steady performance measurements of a turbofan engine with inlet distortions containing co- and counterrotating swirl from an intake diffuser for hypersonic flight
Authors: Schmid, NR Leinhos, DC Fottner, L
Citation: Nr. Schmid et al., Steady performance measurements of a turbofan engine with inlet distortions containing co- and counterrotating swirl from an intake diffuser for hypersonic flight, J TURBOMACH, 123(2), 2001, pp. 379-385
The influence of transient inlet distortions on the instability inception of a low-pressure compressor in a turbofan engine
Authors: Leinhos, DC Schmid, NR Fottner, L
Citation: Dc. Leinhos et al., The influence of transient inlet distortions on the instability inception of a low-pressure compressor in a turbofan engine, J TURBOMACH, 123(1), 2001, pp. 1-8
The use of hot-wire anemometry to investigate unsteady wake-induced boundary-layer development on a high-lift LP turbine cascade
Authors: Wolff, S Brunner, S Fottner, L
Citation: S. Wolff et al., The use of hot-wire anemometry to investigate unsteady wake-induced boundary-layer development on a high-lift LP turbine cascade, J TURBOMACH, 122(4), 2000, pp. 644-650
The influence of technical surface roughness caused by precision forging on the flow around a highly loaded compressor cascade
Authors: Leipold, R Boese, M Fottner, L
Citation: R. Leipold et al., The influence of technical surface roughness caused by precision forging on the flow around a highly loaded compressor cascade, J TURBOMACH, 122(3), 2000, pp. 416-424
Closure to "Discussion of 'The influence of technical surface roughness caused by precision forging on the flow around a highly loaded compressor cascade' " [ASME J. Turbomach., 122, No. 3, p. 424 (2000)]
Authors: Leipold, R Boese, M Fottner, L
Citation: R. Leipold et al., Closure to "Discussion of 'The influence of technical surface roughness caused by precision forging on the flow around a highly loaded compressor cascade' " [ASME J. Turbomach., 122, No. 3, p. 424 (2000)], J TURBOMACH, 122(3), 2000, pp. 425-425
Stall inception in the compressor system of a turbofan engine
Authors: Hoss, B Leinhos, D Fottner, L
Citation: B. Hoss et al., Stall inception in the compressor system of a turbofan engine, J TURBOMACH, 122(1), 2000, pp. 32-44
Three-dimensional flow analysis of turbine blade cascades with leading-edge ejection
Authors: Bohn, D Becker, V Kusterer, K Fottner, L Ardey, S
Citation: D. Bohn et al., Three-dimensional flow analysis of turbine blade cascades with leading-edge ejection, J PROPUL P, 16(1), 2000, pp. 49-56
A numerical study of the influence of grid refinement and turbulence modeling on the flow field inside a highly loaded turbine cascade
Authors: Hildebrandt, T Fottner, L
Citation: T. Hildebrandt et L. Fottner, A numerical study of the influence of grid refinement and turbulence modeling on the flow field inside a highly loaded turbine cascade, J TURBOMACH, 121(4), 1999, pp. 709-716
Controlling the secondary flow in a turbine cascade by three-dimensional airfoil design and endwall contouring
Authors: Duden, A Raab, I Fottner, L
Citation: A. Duden et al., Controlling the secondary flow in a turbine cascade by three-dimensional airfoil design and endwall contouring, J TURBOMACH, 121(2), 1999, pp. 191-199
Risultati: 1-9 |