A New Loss and Deviation Model for Axial Compressor Inlet Guide Vanes (English)
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In:
Transactions of the ASME, Journal of Turbomachinery
;
136
, 7
;
071011/1-071011/13
;
2014
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ISSN:
- Article (Journal) / Print
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Title:A New Loss and Deviation Model for Axial Compressor Inlet Guide Vanes
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Additional title:Neues Modell zur Berechnung der Strömungsumlenkung und -verluste bei der Durchströmung der Einlauf-Leitschaufeln eines Axialverdichters
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Contributors:
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Published in:Transactions of the ASME, Journal of Turbomachinery ; 136, 7 ; 071011/1-071011/13
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Publisher:
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Publication date:2014
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Size:13 Seiten, Bilder, Tabellen, 18 Quellen
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ISSN:
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DOI:
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Type of media:Article (Journal)
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Type of material:Print
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Language:English
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Keywords:
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Source:
Table of contents – Volume 136, Issue 7
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 71001
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On Kinematic Relaxation and Deposition of Water Droplets in the Last Stages of Low Pressure Steam TurbinesStarzmann, J. et al. | 2014
- 71002
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Effect of Nozzle Guide Vane Lean Under Influence of Inlet Temperature TraverseRahim, A. et al. | 2014
- 71003
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Radial Turbine Rotor Response to Pulsating Inlet FlowsCao, Teng et al. | 2014
- 71004
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Aeromechanical Optimization of a Winglet-Squealer Tip for an Axial TurbineSchabowski, Zbigniew et al. | 2014
- 71005
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Modeling Vortex Generating Jet-Induced Transition in Low-Pressure TurbinesHerbst, Florian et al. | 2014
- 71006
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An Experimental Study of Mist/Air Film Cooling on a Flat Plate With Application to Gas Turbine Airfoils—Part I: Heat TransferZhao, Lei et al. | 2014
- 71007
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An Experimental Study of Mist/Air Film Cooling On a Flat Plate With Application to Gas Turbine Airfoils—Part II: Two-Phase Flow Measurements and Droplet DynamicsZhao, Lei et al. | 2014
- 71008
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Development of a Turning Mid Turbine Frame With Embedded Design—Part I: Design and Steady MeasurementsSpataro, Rosario et al. | 2014
- 71009
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Influence of Circumferential Inflow Distortion on the Performance of a Low Speed, High Aspect Ratio Contra Rotating Axial FanMistry, Chetan et al. | 2014
- 71010
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Aerodynamic Interactions Between a High-Pressure Turbine and the First Low-Pressure StatorGougeon, Pierre et al. | 2014
- 71011
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A New Loss and Deviation Model for Axial Compressor Inlet Guide VanesBanjac, Milan et al. | 2014
- 71012
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Development of a Turning Mid Turbine Frame With Embedded Design—Part II: Unsteady MeasurementsSpataro, Rosario et al. | 2014
- 71013
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Parametric Optimization of Unsteady End Wall Blowing on a Highly Loaded Low-Pressure TurbineBenton, Stuart I. et al. | 2014
- 71014
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Influence of Prehistory and Leading Edge Contouring on Aero Performance of a Three-Dimensional Nozzle Guide VaneSaha, Ranjan et al. | 2014
- 74501
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Accuracies of Reduced Order Models of a Bladed Rotor With Geometric MistuningBhartiya, Yasharth et al. | 2014
- 77001
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Erratum: “Tip Clearance Effects on Inlet Hot Streak Migration Characteristics in High Pressure Stage of a Vaneless Counter-Rotating Turbine” [Journal of Turbomachinery, 2010, 132(1), p. 011005]Qingjun, Zhao et al. | 2014