Abstract
One of the major objectives in aircraft engine design is to achieve a high power to weight ratio. Since the weight of the compressor in modern aircraft engines amounts 2/3 of the entire engine, its weight reduction is of high economical interest to aircraft industries.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
De Haller P. (1955) “Das Verhalten von Tragflügelgittern in Axialverdichtem und im Windkanal” VDI-Berichte, Bd. 3
Lieblein S. (1953) “Diffusion Factor for Estimating Loses and Limiting Blade Loadings in Axial Flow Compressor Blade Elements” NACA RM E53D01
Grollius H.W. (1981) “Experimentelle Untersuchung von Rotor Nachlaufdellen und deren Auswirkungen auf die dynamische Belastung axialer Verdichter-und Turbinengitter”, Disseration RWTH Aachen
Schulz H.D. (1989) “Experimentelle Untersuchung der dreidimensionalen abgelösten Strömung in einem Axialverdichterringgitter”, Disseration RWTH Aachen, 1989
Poensgen C.A (1989) “Ein Verfahren zur Vermessung der instationâren dreidimensionalen Strömungsvektoren in Turbomaschinen”, Institut für Strahlantriebe und Turboarbeitsmaschinen RWTH Aachen, Mitteilung Nr. 89–01, 1989
Poensgen C.A. (1991) “Experimentelle Untersuchung der Strömung in einer Unterschall-Axialverdichterstufe bei hoher Drosselung und im Rotating Stall”, Disseration RWTH Aachen, 1991
Schulz H.D., Gallus H.E. (1988) “Experimental Investigations of the Three-Dimensional Flow in an Annular Compressor Cascade”, Journal of Turbomachinery, Vol. 110
Schulz H.D., Gallus H.E., Lakshminarayana B. (1989) “Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction” Part I: Quasi-Steady Flow Field and Comparison with Steady-State Data Part II: Unsteady Flow and Pressure Field Journal of Turbomachinery, Vol. 112
Schulz H.D., Gallus H.E., (1989) “Experimental Investigation of the Influence of Rotor Wakes on the Development of the Profile Boundary Layer and the Performance of an Annular Compressor Cascade” AGARD CPP-468/469, Conference on Unsteady Aerodynamic Phenomena in Turbomachines, Luxembourg 1989
Poensgen C.A., Gallus H.E. (1990) “Three-Dimensional Wake Decay Inside of a Compressor Cascade and its Influence on the Downstream Unsteady Flow Field” Part I: Wake Decay Characteristics in the Flow Passage Part II: Unsteady Flow Field Downstream of the Stator Journal of Turbomachinery, Vol 113, April 1991, pp 180 ff
Gallus H.E., Hah C., Schulz H.D. (1990) “Experimental and Numerical Investigation of Three-Dimensional Viscous Flows and Vortex Motion inside an Annular Compressor Blade Row” Journal of Turbomchinery, Vol. 113, April 1991
Joslyn H.D., Dring R.P., (1985) “Axial Compressor Stator Aerodynamics”, Journal of Engineering for Gas Turbines and Power, Vol 107
Dong Y., Gallimore S.J., Hodson H.P., (1987) “Three-Dimensional Flows and Loss Reduction in Axial Compressors” Journal of Turbomachinery, Vol. 109
Author information
Authors and Affiliations
Editor information
Rights and permissions
Copyright information
© 1993 Springer Fachmedien Wiesbaden
About this chapter
Cite this chapter
Gallus, H.E., Schulz, M.D., Poensgen, C.A. (1993). Experimental Investigation of the Three-Dimensional Separated Flow in an Annular Compressor Cascade. In: Gersten, K. (eds) Physics of Separated Flows — Numerical, Experimental, and Theoretical Aspects. Notes on Numerical Fluid Mechanics (NNFM), vol 40. Vieweg+Teubner Verlag, Wiesbaden. https://doi.org/10.1007/978-3-663-13986-7_35
Download citation
DOI: https://doi.org/10.1007/978-3-663-13986-7_35
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
Print ISBN: 978-3-531-07640-9
Online ISBN: 978-3-663-13986-7
eBook Packages: Springer Book Archive