The effect of leading-edge geometry on wake interactions in compressors (Englisch)
- Neue Suche nach: Wheeler, Andrew P.S.
- Neue Suche nach: Sofia, Alessandro
- Neue Suche nach: Miller, Robert J.
- Neue Suche nach: Wheeler, Andrew P.S.
- Neue Suche nach: Sofia, Alessandro
- Neue Suche nach: Miller, Robert J.
In:
Transactions of the ASME, Journal of Turbomachinery
;
131
, 4
;
041013/1-041013/8
;
2009
-
ISSN:
- Aufsatz (Zeitschrift) / Print
-
Titel:The effect of leading-edge geometry on wake interactions in compressors
-
Beteiligte:
-
Erschienen in:Transactions of the ASME, Journal of Turbomachinery ; 131, 4 ; 041013/1-041013/8
-
Verlag:
-
Erscheinungsdatum:2009
-
Format / Umfang:8 Seiten, 16 Bilder, 14 Quellen
-
ISSN:
-
DOI:
-
Medientyp:Aufsatz (Zeitschrift)
-
Format:Print
-
Sprache:Englisch
-
Schlagwörter:
-
Datenquelle:
Inhaltsverzeichnis – Band 131, Ausgabe 4
Zeige alle Jahrgänge und Ausgaben
Die Inhaltsverzeichnisse werden automatisch erzeugt und basieren auf den im Index des TIB-Portals verfügbaren Einzelnachweisen der enthaltenen Beiträge. Die Anzeige der Inhaltsverzeichnisse kann daher unvollständig oder lückenhaft sein.
- 41001
-
Boundary Layer Separation Control With Fluidic OscillatorsCerretelli, Ciro et al. | 2009
- 41002
-
Superposition Predictions of the Reduction of Hot Streaks by Coolant From a Film-Cooled Guide VaneJenkins, Sean C. et al. | 2009
- 41003
-
Prediction of Film Cooling and Heat Transfer on a Rotating Blade Platform With Stator-Rotor Purge and Discrete Film-Hole Flows in a 1-fraction SHAPE="CASE">12 Turbine StageYang, H. et al. | 2009
- 041003
-
Prediction of Film Cooling and Heat Transfer on a Rotating Blade Platform With Stator-Rotor Purge and Discrete Film-Hole Flows in a 1- 1/2 Turbine StageYang, H. / Gao, Z. / Chen, H.C. / Han, J.C. / Schobeir, M.T. et al. | 2009
- 41004
-
Turbine Blade Platform Film Cooling With Typical Stator-Rotor Purge Flow and Discrete-Hole Film CoolingGao, Zhihong et al. | 2009
- 41005
-
Heat Transfer Coefficients of Film Cooling on a Rotating Turbine Blade Model-Part I: Effect of Blowing RatioTao, Zhi et al. | 2009
- 41007
-
Film-Cooling Flowfields With Trenched Holes on an EndwallSundaram, N. et al. | 2009
- 41008
-
The Effects of Aerodynamic Asymmetric Perturbations on Forced Response of Bladed DisksMiyakozawa, Tomokazu et al. | 2009
- 41009
-
Investigations on the Discharge and Total Temperature Increase Characteristics of the Labyrinth Seals With Honeycomb and Smooth LandsYan, Xin et al. | 2009
- 41010
-
Sensitization of the SST Turbulence Model to Rotation and Curvature by Applying the Spalart-Shur Correction TermSmirnov, Pavel E. et al. | 2009
- 41011
-
Effect of Unsteadiness on the Performance of a Transonic Centrifugal Compressor StageTre´binjac, Isabelle et al. | 2009
- 41012
-
Effect of Wakes and Secondary Flow on Re-attachment of Turbine Exit Annular Diffuser FlowKluß, David et al. | 2009
- 41013
-
The Effect of Leading-Edge Geometry on Wake Interactions in CompressorsWheeler, Andrew P.S. et al. | 2009
- 41014
-
Shorten the Intermediate Turbine Duct Length by Applying an Integrated ConceptMarn, A. et al. | 2009
- 41015
-
Aerothermal Performance of Streamwise and Compound Angled Pulsating Film Cooling JetsAga, Vipluv et al. | 2009
- 41016
-
Influence of Wake Structure on Unsteady Flow in a Low Pressure Turbine Blade PassageSarkar, S. et al. | 2009
- 41017
-
Heat Transfer in Leading Edge, Triangular Shaped Cooling Channels With Angled Ribs Under High Rotation NumbersLiu, Yao-Hsien et al. | 2009
- 41018
-
The Effects of Manufacturing Tolerances on Gas Turbine CoolingBunker, Ronald S. et al. | 2009
- 41019
-
Windage Power Losses From Spiral Bevel Gears With Varying Oil Flows and Shroud ConfigurationsJohnson, Graham et al. | 2009
- 41020
-
Simplified Approach to Predicting Rough Surface TransitionBoyle, R.J. et al. | 2009
- 44501
-
Experimental Study of Heat Transfer Augmentation Near the Entrance to a Film Cooling Hole in a Turbine Blade Cooling PassageScheepers, Gerard et al. | 2009