Analysis of Unsteady Secondary Flows in Linear Low-pressure Turbine Cascades

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ISBN 13 : 9783843935647
Total Pages : pages
Book Rating : 4.9/5 (356 download)

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Book Synopsis Analysis of Unsteady Secondary Flows in Linear Low-pressure Turbine Cascades by : Roberto Ciorciari

Download or read book Analysis of Unsteady Secondary Flows in Linear Low-pressure Turbine Cascades written by Roberto Ciorciari and published by . This book was released on 2018 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Direct Numerical Simulations of the Unsteady Secondary Flow in the Near-wall Region of a Linear Low Pressure Turbine Cascade

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ISBN 13 : 9783959081665
Total Pages : pages
Book Rating : 4.0/5 (816 download)

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Book Synopsis Direct Numerical Simulations of the Unsteady Secondary Flow in the Near-wall Region of a Linear Low Pressure Turbine Cascade by : Denis Koschichow

Download or read book Direct Numerical Simulations of the Unsteady Secondary Flow in the Near-wall Region of a Linear Low Pressure Turbine Cascade written by Denis Koschichow and published by . This book was released on 2019 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Visualization Study of Secondary Flows in Cascades

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ISBN 13 :
Total Pages : 106 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis A Visualization Study of Secondary Flows in Cascades by : Arthur G. Hansen

Download or read book A Visualization Study of Secondary Flows in Cascades written by Arthur G. Hansen and published by . This book was released on 1953 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flow-visualization techniques are employed to ascertain the streamline patterns of the nonpotential, secondary flows in the boundary layers of cascades, thereby providing a basis for more extended analyses in turbomachines. The three-dimensional deflection of the end-wall boundary layer results in the formation of a vortex well up in each cascade passage. The size and tightness of the vortex generated depend upon the main flow turning in the cascade passage. Once formed, a vortex resists turning in subsequent blade rows. This results in unfavorable angles of attack and possible flow disturbances on the pressure surfaces of subsequent blade rows when the vortices impinge on these surfaces.

An Analysis of Losses and Secondary Flow in Turbine Cascades

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ISBN 13 :
Total Pages : 81 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis An Analysis of Losses and Secondary Flow in Turbine Cascades by : W. Hosny

Download or read book An Analysis of Losses and Secondary Flow in Turbine Cascades written by W. Hosny and published by . This book was released on 1971 with total page 81 pages. Available in PDF, EPUB and Kindle. Book excerpt: A general review of different cascade losses is presented with emphasis on the secondary flow. An analytical analysis utilizing the Squire and Winter secondary flow analysis along with the triangle model for end wall boundary layer proposed by Taylor is detailed in an attempt to show the behavior of streamlines near the end wall. (Author).

Simulation of Flow Through Low-pressure Linear Turbine Cascade, Using Multi-block Structured Grid

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (546 download)

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Book Synopsis Simulation of Flow Through Low-pressure Linear Turbine Cascade, Using Multi-block Structured Grid by :

Download or read book Simulation of Flow Through Low-pressure Linear Turbine Cascade, Using Multi-block Structured Grid written by and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: The Reynolds number for the flow through LPT at cruise conditions is much lower than that at the take-off conditions. This low-Re flow has a great tendency to undergo separation on the suction surface of the turbine blade when an adverse pressure gradient is encountered. This prevailing flow separation is detrimental to the performance of the LPT. Hence, low-pressure turbine (LPT) stage in aircraft engines undergo significant losses during cruise conditions. Therefore, accurate prediction of flow separation is crucial for an effective design of LPT blade, and is achieved in the present work using a high-order accurate numerical solution procedure. The accurate prediction of flow separation is necessary for implementing flow control techniques, passive or active, to possibly delay or prevent the occurrence of flow separation in the low-pressure turbine stage in an aircraft engine. A multi-block, periodic, structured grid of multiple topologies generated by the grid generation software, GRIDPRO, is used for the present numerical analysis. The three-dimensional, unsteady, full Navier-Stokes equations are solved to analyze the flow. A MPI-based higher-order, parallel, chimera Large-Eddy Simulation (LES), version of the FDL3DI flow solver, developed by the Air Force Research Laboratory at Wright Patterson Air Force Base, is extended for the present turbo-machinery application. A sixth-order accurate compact-difference scheme is usual for the spatial discretization, coupled with tenth-order filtering to minimize the numerical oscillations in the flow solution and maintain numerical stability, along with second-order accurate temporal discretization. Also examined is the effect of grid density and the location of the upstream inflow boundary ... Finally, the baseline simulation study of flow over a circular cylinder at ReD = 13,400 is performed as a starting step for the future study of implementation of flow control techniques for preventing or delaying the flow separation.

On the Unsteady Secondary Flow Inside a Low Pressure Turbine Stage

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ISBN 13 : 9783844036046
Total Pages : 114 pages
Book Rating : 4.0/5 (36 download)

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Book Synopsis On the Unsteady Secondary Flow Inside a Low Pressure Turbine Stage by : Carsten Schneider

Download or read book On the Unsteady Secondary Flow Inside a Low Pressure Turbine Stage written by Carsten Schneider and published by . This book was released on 2014 with total page 114 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Unsteady Secondary Flow in an Engine-Representative Low Pressure Turbine

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ISBN 13 : 9783843921046
Total Pages : 117 pages
Book Rating : 4.9/5 (21 download)

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Book Synopsis Unsteady Secondary Flow in an Engine-Representative Low Pressure Turbine by : Daniel Schrack

Download or read book Unsteady Secondary Flow in an Engine-Representative Low Pressure Turbine written by Daniel Schrack and published by . This book was released on 2015 with total page 117 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect of Incidence on Secondary Flows in a Linear Turbine Cascade

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (137 download)

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Book Synopsis Effect of Incidence on Secondary Flows in a Linear Turbine Cascade by : G. V. Ramana Murty

Download or read book Effect of Incidence on Secondary Flows in a Linear Turbine Cascade written by G. V. Ramana Murty and published by . This book was released on 1994 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Secondary Flows and Losses in a Turbine Cascade

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (228 download)

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Book Synopsis Secondary Flows and Losses in a Turbine Cascade by : D. G. Gregory-Smith

Download or read book Secondary Flows and Losses in a Turbine Cascade written by D. G. Gregory-Smith and published by . This book was released on 1983 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: In designing axial flow turbines, one needs relatively simple prediction techniques for the angle variations and losses produced by secondary flows. To improve the physical basis of such techniques, an investigation was made of the flow in a cascade of large scale rotor blades of some 110 deg of turning. The aspect around 0.2 of the span. The flow was traversed in great detailed on ten planes using cobra-type probes with a computerised data recording and analysis system. Results are presented graphically using contour and vector plots on various planes through the flow field. The horse-show vortex and passage vortex development are clearly seen, with the upstream boundary layer being shed downstream as a loss core. Another region of high loss is related to a counter vortex in the corner between the sunction surface and the end wall. Results were also pitch averaged, and compared with predictions of angle and loss distribution. Some traversing was carried out using hot wire anemometry. Regions of high turbulence intensity and shear stress were identified, associated with the regions of high loss. Some indication is given of the mechanisms of loss production within the cascade.

Controlling Secondary Flows in Very Highly-loaded Low-pressure Turbine Cascades

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ISBN 13 :
Total Pages : 546 pages
Book Rating : 4.:/5 (811 download)

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Book Synopsis Controlling Secondary Flows in Very Highly-loaded Low-pressure Turbine Cascades by : Daniel C. Knezevici

Download or read book Controlling Secondary Flows in Very Highly-loaded Low-pressure Turbine Cascades written by Daniel C. Knezevici and published by . This book was released on 2012 with total page 546 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Comparison of steady and unsteady secondary flows in a turbine stator cascade

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (137 download)

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Book Synopsis Comparison of steady and unsteady secondary flows in a turbine stator cascade by : Gregory John Hebert

Download or read book Comparison of steady and unsteady secondary flows in a turbine stator cascade written by Gregory John Hebert and published by . This book was released on 1988 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Secondary Flow Reduction Techniques in Linear Turbine Cascades

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ISBN 13 :
Total Pages : 426 pages
Book Rating : 4.:/5 (257 download)

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Book Synopsis Secondary Flow Reduction Techniques in Linear Turbine Cascades by : Thomas Ernst Biesinger

Download or read book Secondary Flow Reduction Techniques in Linear Turbine Cascades written by Thomas Ernst Biesinger and published by . This book was released on 1993 with total page 426 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Theoretical and Experimental Study on Periodic Unsteady Wake Development, Unsteady Boundary Layer Development, and Trailing Edge Ejection Mixing Loss Optimization in a Linear Turbine Cascade

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ISBN 13 :
Total Pages : 492 pages
Book Rating : 4.:/5 (394 download)

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Book Synopsis Theoretical and Experimental Study on Periodic Unsteady Wake Development, Unsteady Boundary Layer Development, and Trailing Edge Ejection Mixing Loss Optimization in a Linear Turbine Cascade by : Kameswara Rao Pappu

Download or read book Theoretical and Experimental Study on Periodic Unsteady Wake Development, Unsteady Boundary Layer Development, and Trailing Edge Ejection Mixing Loss Optimization in a Linear Turbine Cascade written by Kameswara Rao Pappu and published by . This book was released on 1997 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt:

High-order Accurate Solution for Flow Through a Turbine Linear Cascade

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (532 download)

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Book Synopsis High-order Accurate Solution for Flow Through a Turbine Linear Cascade by :

Download or read book High-order Accurate Solution for Flow Through a Turbine Linear Cascade written by and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Low-pressure turbines (LPT) in aircraft engines undergo tremendous losses at cruise conditions. The flow Reynolds number at cruise is lower than the take-off Reynolds number by a factor of almost two. At low Reynolds numbers, the flow is largely laminar, and tends to separate easily on the suction surface of the turbine blade when an adverse pressure gradient is encountered. Therefore, accurate prediction of flow separation is crucial for an effective design of LPT blade; and is achieved in the present work using a high-order accurate numerical solution procedure. The three-dimensional, unsteady, full Navier-Stokes equations are solved to analyze the flow. A MPI-based higher-order, parallel, chimera version of the FDL3DI flow solver, is extended for use with this turbomachinery application. A sixth-order accurate compact-difference scheme is used for the spatial discretization, along with second-order accurate temporal discretization. Tenth-order filtering is used to minimize the numerical oscillations in the flow solution and maintain numerical stability. The objective of the present study is to show the ability of higher-order accurate compact-difference scheme to predict the flow separation that occurs inside an LPT cascade at Re C = 25,000 (based on axial chord and inlet velocity). A new set of subsonic inflow/outflow boundary conditions that account for upstream influence (BC2) are derived by specifying stagnation quantities at the inlet, and a static quantity at the exit of the flow domain, and maintaining the inflow angle constant. For inflow/outflow boundary conditions that do not account for upstream influence, fixed inflow with extrapolated outflow (BC1) has been utilized. The effect of the two different sets of inflow/outflow boundary conditions on the flow solution is studied, for second-order, fourth-order and sixth-order accurate schemes. The computed Cp distribution for the LPT flow shows good agreement with the existing experimental data. The location of the onset of separation matches with an available LES simulation result and with the available experimental data. The performance of high-order compact difference schemes has been assessed via simulation of laminar flow over a circular cylinder at Re D = 250 (based on free-stream velocity and cylinder diameter). The sixth-order accurate compact difference scheme with tenth-order filtering on a coarser mesh preserves the vortex structure better than possible with the second-order accurate scheme on a finer mesh. This demonstrates the efficiency of the higher-order accurate compact difference scheme.

Analysis of Separated Flow in a Low-pressure Turbine Linear Cascade, Using Multi-block Structured Grid

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Analysis of Separated Flow in a Low-pressure Turbine Linear Cascade, Using Multi-block Structured Grid by : Pavan K. Mutnuri

Download or read book Analysis of Separated Flow in a Low-pressure Turbine Linear Cascade, Using Multi-block Structured Grid written by Pavan K. Mutnuri and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Direct and Large Eddy Simulation XIII

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Publisher : Springer Nature
ISBN 13 : 3031470281
Total Pages : 389 pages
Book Rating : 4.0/5 (314 download)

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Book Synopsis Direct and Large Eddy Simulation XIII by : Cristian Marchioli

Download or read book Direct and Large Eddy Simulation XIII written by Cristian Marchioli and published by Springer Nature. This book was released on 2023-11-15 with total page 389 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book covers the diverse and cutting-edge research presented at the 13th ERCOFTAC Workshop on Direct and Large Eddy Simulation. The first section of the book focuses on Aerodynamics/Aeroacoustics, comprising eight papers that delve into the intricate relationship between fluid flow and aerodynamic performance. The second section explores the dynamics of Bluff/Moving Bodies through four insightful papers. Bubbly Flows, the subject of the third section, is examined through four papers. Moving on, the fourth section is dedicated to Combustion and Reactive Flows, presenting two papers that focus on the complex dynamics of combustion processes and the interactions between fluids and reactive species. Convection and Heat/Mass Transfer are the central themes of the fifth section, which includes three papers. These contributions explore the fundamental aspects of heat and mass transfer in fluid flows, addressing topics such as convective heat transfer, natural convection, and mass transport phenomena. The sixth section covers Data Assimilation and Uncertainty Quantification, featuring two papers that highlight the importance of incorporating data into fluid dynamic models and quantifying uncertainties associated with these models. The subsequent sections encompass a wide range of topics, including Environmental and Industrial Applications, Flow Separation, LES Fundamentals and Modelling, Multiphase Flows, and Numerics and Methodology. These sections collectively present a total of 23 papers that explore different facets of fluid dynamics, contributing to the advancement of the field and its practical applications.

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 704 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt: