Aerodynamic Performance of Turbine Center Frames With Purge Flows—Part I: The Influence of Turbine Purge Flow Rates

2018 ◽  
Vol 140 (6) ◽  
Author(s):  
Stefan Zerobin ◽  
Andreas Peters ◽  
Sabine Bauinger ◽  
Ashwini Bhadravati Ramesh ◽  
Michael Steiner ◽  
...  
Keyword(s):  
Measurement Data ◽  
Leading Edge ◽  
Aerodynamic Performance ◽  
Flow Structures ◽  
Flow Rates ◽  
Purge Flow ◽  
Mass Flows ◽  
The Individual ◽  
The Impact ◽  
First Time

This two-part paper deals with the influence of high-pressure turbine (HPT) purge flows on the aerodynamic performance of turbine center frames (TCF). Measurements were carried out in a product-representative one and a half-stage turbine test setup. Four individual purge mass flows differing in flow rate, pressure, and temperature were injected through the hub and tip, forward and aft cavities of the unshrouded HPT rotor. Two TCF designs, equipped with nonturning struts, were tested and compared. In this first part of the paper, the influence of different purge flow rates (PFR) is discussed, while in the second part of the paper, the impact of the individual hub and tip purge flows on the TCF aerodynamics is investigated. The acquired measurement data illustrate that the interaction of the ejected purge flow with the main flow enhances the secondary flow structures through the TCF duct. Depending on the PFR, the radial migration of purge air onto the strut surfaces directly impacts the loss behavior of the duct. The losses associated with the flow close to the struts and in the strut wakes are highly dependent on the relative position between the HPT vane and the strut leading edge (LE), as well as the interaction between vane wake and ejected purge flow. This first-time experimental assessment demonstrates that a reduction in the purge air requirement benefits the engine system performance by lowering the TCF total pressure loss.

Aerodynamic Performance of Turbine Center Frames With Purge Flows—Part II: The Influence of Individual Hub and Tip Purge Flows

2018 ◽  
Vol 140 (6) ◽  
Author(s):  
Stefan Zerobin ◽  
Christian Aldrian ◽  
Andreas Peters ◽  
Franz Heitmeir ◽  
Emil Göttlich
Keyword(s):  
High Pressure ◽  
Operating Conditions ◽  
High Pressure Turbine ◽  
Flow Rates ◽  
Purge Flow ◽  
Flow Evolution ◽  
Generation Mechanisms ◽  
The Impact ◽  
First Time ◽  
Time Assessment

The aerodynamic behavior of turbine center frame (TCF) ducts under the presence of high-pressure turbine (HPT) purge flows was experimentally investigated in this two-part paper. While the first part of the paper demonstrated the impact of varying the purge flow rates (PFR) on the loss behavior of two different TCF designs, the second part concentrates on the influence of individual hub and tip purge flows on the main flow evolution and loss generation mechanisms through the TCF ducts. Therefore, measurements were conducted at six different operating conditions in a one and a half stage turbine test setup, featuring four individual purge flows injected through the hub and tip, forward and aft cavities of the HPT rotor. The outcomes of this first-time assessment indicate that a HPT purge flow reduction generally benefits TCF performance. Decreasing one of the rotor case PFRs leads to an improved duct pressure loss. The purge flows from the rotor aft hub and tip cavities are demonstrated to play a particularly important role for improving the duct aerodynamic behavior. In contrast, the forward rotor hub purge flow actually stabilizes the flow in the TCF duct and reducing this purge flow can penalize TCF performance. These particular HPT/TCF interactions should be taken into account whenever high-pressure turbine purge flow reductions are pursued.

Trust, Ethnicity and Integrity in East Africa: Experimental Evidence from Kenya and Tanzania

2017 ◽  
Vol 2 (1) ◽  
pp. 88-123 ◽  
Author(s):  
Dominic Burbidge ◽  
Nic Cheeseman
Keyword(s):  
Ethnic Diversity ◽  
Negative Impact ◽  
Common Knowledge ◽  
Individual Level ◽  
Trust Games ◽  
Negative Effect ◽  
Experimental Games ◽  
The Individual ◽  
The Impact ◽  
First Time

AbstractPolitical economy comparisons of Kenya and Tanzania have often found the political salience of ethnicity to be far higher in the former than the latter, with a negative impact on intercommunal trust. This difference has tended to be explained on the basis of the different kinds of leadership that the two countries experienced after independence. However, these findings have typically been demonstrated using aggregate or survey data. This paper assesses the salience of ethnicity at the individual level for the first time, deploying monetized two-round trust games in urban Kenya and Tanzania. The experimental games isolate the comparative impact of common knowledge of ethnicity and integrity among a quasi-random selection of 486 citizens. Verifying previous findings, we observe higher levels of trust and trustworthiness in Tanzania as compared with Kenya. Further, in comparison with Kenya, any shared knowledge of ethnic identities in Tanzania leads players to transfer fewer resources, while common knowledge that both players are “honest” led to higher transfers there than in Kenya. These results provide robust evidence of higher levels of trust in Tanzania, and of the negative effect in that country of common knowledge of ethnicity on levels of cooperation. The findings demonstrate the way in which political context can shape the impact of ethnic diversity, and encourage further experimental research that looks at the intersubjective dynamics of social cooperation.

Experimental analysis of cell pattern on grid fin aerodynamics in subsonic flow

2019 ◽  
Vol 234 (3) ◽  
pp. 537-562
Author(s):  
Manish Tripathi ◽  
Mahesh M Sucheendran ◽  
Ajay Misra
Keyword(s):  
Subsonic Flow ◽  
Lift Coefficient ◽  
Aerodynamic Performance ◽  
Aerodynamic Efficiency ◽  
Grid Fin ◽  
Stall Angle ◽  
The Individual ◽  
The Impact ◽  
Control Surfaces

Grid fins consisting of a lattice of high aspect ratio planar members encompassed by an outer frame are unconventional control surfaces used on numerous missiles and bombs due to their enhanced lifting characteristics at high angles of attack and across wider Mach number regimes. The current paper accomplishes and compares the effect of different grid fin patterns on subsonic flow aerodynamics of grid fins by virtue of the determination of their respective aerodynamic forces. Furthermore, this study deliberates the impact of gap variation on aerodynamics of different patterns. Results enunciate enhanced aerodynamic efficiency, and lift slope for web-fin cells and single diamond patterns compared to the baseline model. Moreover, the study indicates improved aerodynamic performance for diamond patterns with higher gaps by providing elevated maximum lift coefficient, delayed stall angle, and comparable drag at lower angles. The study established the presence of an additional effect termed as the inclination effect alongside the cascade effect leading to deviations with respect to lift, stall, and aerodynamic efficiency amongst different gap variants of the individual patterns. Thus, optimization based on the aerodynamic efficiency, stall angle requirements, and construction cost by optimum pattern and gap selection can be carried out through this analysis, which can lead to elevated aerodynamic performance for grid fins.

scholarly journals TYPES OF INDIVIDUAL WOMEN EROTIC CODE

2018 ◽  
Keyword(s):  
Life Experience ◽  
Married Couples ◽  
Professional Activity ◽  
Self Reflection ◽  
Early Life Experience ◽  
New Material ◽  
Definition Of ◽  
The Individual ◽  
The Impact ◽  
First Time

The article is devoted to the current issue of sexuality. Significant expansion and development of psychologists’ professional activity necessitate creating of generalized classification of individuals and married couples’ behavioral erotic types. The destruction of self-reflection, self-perception and the difficulty of interpersonal understanding are due to the substitution of concepts. The study of sexual-psychological characteristics of behavioral patterns of women in erotic relationships is very important in this regard. The new material on the topic under study is generalized. Erotic imagination functions and erotic images impact on the process of forming a fixed erotic Image of a sexual partner in women are determined. The impact of early life experience (imprinting) influenced on the individual erotic code formation is determined. Several motivational schemes of sexual behavior are described. Authors submit the definition of «individual erotic code» for the first time. «Individual erotic code» is found out as the unified recording system of the individual model erotic behavior and her «ideal partner» reactions on this behavior. The types of women individual erotic code, based on the concept of archetypes (K.G. Jung, D. S. Bolen) study are defined. Types of individual erotic code were named after the ancient Greek goddesses: Artemis, Athena, Hestia, Hera, Demeter, Persephone, Aphrodite. The attention is focused on the deep analysis of individual women erotic code stages realization, such as, the genesis of erotic impulse, the tempting process, the sexual act behavior, the pregnancy, the caring of posterity. Materials of research can be used in the practical work of psychologists and psychotherapists which working both with married couples, as well as in individual work with the client.

The Behavior of Turbine Center Frames Under the Presence of Purge Flows

2017 ◽  
Author(s):  
S. Zerobin ◽  
A. Peters ◽  
S. Bauinger ◽  
A. Ramesh ◽  
M. Steiner ◽  
...  
Keyword(s):  
High Pressure ◽  
Secondary Flow ◽  
Pressure Loss ◽  
Measurement Data ◽  
Leading Edge ◽  
Turbine Rotor ◽  
High Pressure Turbine ◽  
Oil Flow ◽  
Purge Flow ◽  
Cooling Air

This paper deals with the influence of high-pressure turbine purge flows on the aerodynamic performance of turbine center frames. Measurements were carried out in a product-representative one and a half stage turbine test setup, installed in the Transonic Test Turbine Facility at Graz University of Technology. The rig allows testing at engine-relevant flow conditions, matching Mach, Reynolds, and Strouhal number at the inlet of the turbine center frame. Four individual purge mass flows differing in flow rate, pressure, and temperature were injected through the hub and tip, forward and aft cavities of the unshrouded high-pressure turbine rotor. Two turbine center frame designs (differing in area distribution and inlet-to-exit radial offset), equipped with non-turning struts, were tested and compared. For both configurations, aerodynamic measurements at the duct inlet and outlet as well as oil flow visualizations through the turbine center frame were performed. The acquired measurement data illustrate that the interaction of the ejected purge flow with the main flow enhances the secondary flow structures through the turbine center frame duct. Depending on the purge flow rates, the radial migration of purge air onto the strut surfaces directly impacts the loss behavior of the duct. While the duct loss is demonstrated to be primarily driven by the core flow between two duct struts, the losses associated with the flow close to the struts and in the strut wakes are highly dependent on the relative position between the high-pressure turbine vane and the strut leading edge, as well as the interaction between vane wake and ejected purge flow. Hence, while the turbine center frame duct pressure loss depends on the duct geometric characteristics it is also influenced by the presence and rate of the high-pressure turbine purge flows. This first-time experimental assessment demonstrates that a reduction in the high-pressure turbine purge and cooling air requirement not only benefits the engine system performance by decreasing the secondary flow taken from the high-pressure compressor but also by lowering the turbine center frame total pressure loss.

scholarly journals Reynolds number influence on the formation of vortical structures on a pitching flat plate

2017 ◽  
Vol 7 (1) ◽  
pp. 20160079 ◽  
Author(s):  
Alexander Widmann ◽  
Cameron Tropea
Keyword(s):  
Boundary Layer ◽  
Reynolds Number ◽  
Leading Edge ◽  
Boundary Layer Separation ◽  
Flow Structures ◽  
Flat Plates ◽  
Time Resolved ◽  
Flow Phenomena ◽  
Wall Interaction ◽  
The Impact

The impact of chord-based Reynolds number on the formation of leading-edge vortices (LEVs) on unsteady pitching flat plates is investigated. The influence of secondary flow structures on the shear layer feeding the LEV and the subsequent topological change at the leading edge as the result of viscous processes are demonstrated. Time-resolved velocity fields are measured using particle image velocimetry simultaneously in two fields of view to correlate local and global flow phenomena in order to identify unsteady boundary-layer separation and the subsequent flow structures. Finally, the Reynolds number is identified as a parameter that is responsible for the transition in mechanisms leading to LEV detachment from an aerofoil, as it determines the viscous response of the boundary layer in the vortex–wall interaction.

A Comparison of a Mono, Twin and Double Scroll Turbine for Automotive Applications

2015 ◽  
Author(s):  
Jason Walkingshaw ◽  
Georgios Iosifidis ◽  
Tobias Scheuermann ◽  
Dietmar Filsinger ◽  
Nobuyuki Ikeya
Keyword(s):  
Mass Flow ◽  
Flow Characteristics ◽  
High Mass ◽  
Flow Rates ◽  
Engine Simulation ◽  
Engine Model ◽  
Trade Offs ◽  
Mass Flow Rates ◽  
The Individual ◽  
The Impact

As a means of meeting ever increasing emissions and fuel economy demands car manufacturers are using aggressive engine downsizing. To maintain the power output of the engine turbocharging is typically used. Due to the miss-match of the mass flow characteristics of the engine to the turbocharger, at low engine mass flow rates, the turbocharger can suffer from slow response known as “Turbolag”. Mono-scroll turbines are capable of providing good performance at high mass flow rates and in conjunction with low inertia mixed flow turbines can offer some benefits for transient engine response. With a multi-entry system the individual volute sizing can be matched to the single mass flow pulse from the engine cylinders. The exhaust pulse energy can be better utilised by the turbocharger turbine improving turbocharger response, while the interaction of the engine exhaust pulses can be better avoided, improving the scavenging of the engine. The behaviour of a mono-scroll turbocharger with the engine using engine simulation tools has been well established. What requires further investigation is the comparison with multi-entry turbines. CFD (Computational Fluid Dynamics) has been used to examine the single admission behaviour of a twin and double scroll turbine. Turbocharger gas stand maps of the multi-entry turbines have been measured at full and single admission. This data has been used in a 0D engine model. In addition, the turbine stage has been tested on the engine and a validation of the engine model against the engine test data is presented. Using the validated engine model a comparison has been made to understand the differences in the sizing requirements of the turbine and the interaction of the mono-scroll and multi-entry turbines with the engine. The impact of the different efficiency and mass flow rate trends of the mono and multi-entry turbochargers are discussed and the trade-offs between the design configurations regarding on engine behaviour are investigated.

scholarly journals Leisure in the context of art practices

2021 ◽  
Author(s):  
Yuliya Tarasenko
Keyword(s):  
Interdisciplinary Research ◽  
Research Work ◽  
Personal Characteristics ◽  
Social Situation ◽  
Science Practices ◽  
Art Research ◽  
The Individual ◽  
Questionnaire Method ◽  
The Impact ◽  
First Time

The purpose of the article. The article is devoted to the characteristics of leisure in the context of art science practices as a factor in the development of the emotional, intellectual and cultural potential of the individual and society. The expansion of the opportunities regarding substantiation of the impact of art science practices at the intersection of art research and neuroscience. The methodology is based on the interdisciplinary method, which involves the study of issues in the interaction and synthesis of knowledge of neuroscience and art history, which allows obtaining new fundamental results and combine them into a general scientific picture of the world, questionnaire method, which consists in finding and studying new knowledge, which carried out during the survey in research work at the School of Art Experts, method of generalization, which revealed a common worldview paradigm. The scientific novelty for the first time, the issue of leisure was discovered and synthesized in the context of research with the involvement of research conducted in the field of neuroscience, indicated in the works of neurobiologists. For the first time, the analysis of interdisciplinary research is carried out and the mechanism of influence is defined to art studies, in particular the influence on the emotional, intellectual and social situation of the individual. Conclusions. Leisure through the art science practice occupies an intermediate place between personal experience and education, accumulating knowledge about the surrounding world of visual forms. Art science practices, as a system of development through creative kinds of leisure, indicate its synergistic aspects, which are embodied in the socio-personal characteristics of a modern individual. The analysis of interdisciplinary research, in particular neuroscience, determined and substantiated the powerful influence of art science practices on the development of not only the emotional and intellectual potential of a person, but also on the development of the brain and mental activity.

Visualization and Analysis of Venting From a Single Microchannel Two-Phase Copper Heat Exchanger

2009 ◽  
Author(s):  
Milnes P. David ◽  
Julie Steinbrenner ◽  
Josef Miler ◽  
Kenneth E. Goodson
Keyword(s):  
Vapor Phase ◽  
Liquid Flow ◽  
Air Injection ◽  
Flow Structures ◽  
Static System ◽  
Two Phase ◽  
Flow Rates ◽  
System Pressure ◽  
The Impact ◽  
Injection Rates

Two-phase microfluidic cooling solutions have the potential to meet the thermal and geometric requirements of high performance microprocessors. However, rapid nucleation and growth of the vapor phase in the micro-scale flow structures produce detrimental rise in the system pressure and create flow instabilities. In our previous work we developed a novel solution to these problems: to locally vent the vapor formed in the microstructures by capping the flow structures with porous, hydrophobic membranes that allow only the trapped vapor phase to escape the system. In this paper we present the results from a visualization study of this venting process in a copper microchannel with a porous hydrophobic Teflon membrane wall and determine the impact of varying flow conditions on the venting process. We tested liquid flow rates of 0.1, 0.25 and 0.5 ml/min with air injection rates varying from 0.2 to 6 ml/min, corresponding to mass qualities of 0.1% to 7%. Bubbly/slug and wavy flows are dominant at the lower liquid and air flow rates, with wavy-stratified and stratified flows becoming dominant at higher air injection rates. At the highest liquid flow rate, plug and annular flows were common. Analysis finds that venting effectiveness is insensitive to Reliq until the point where non-contact flow structures such as annular become dominant and result in a loss of effective venting area. We also find that venting area changes linearly with mass quality and that the maximum venting effectiveness can be improved by increasing the venting area or raising the total static system pressure. However, venting effectiveness is fundamentally limited by the membrane conductance.

Sign in / Sign up

Export Citation Format

Share Document