CFD Events Calendar, Event Record #1312
ADVANCES IN TURBOMACHINERY AERO-THERMO-MECHANICAL DESIGN AND ANALYSIS
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The present multidisciplinary Lecture Series addresses the
current state of the art in the design and analysis of
axial Turbomachinery components.
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Date: |
November 27, 2007 - November 30, 2007
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Location: |
Wright patterson Air Force base at the Wright State University, Dayton, Ohio, United States
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Web Page: |
http://www.vki.ac.be/educat/lect-ser/index.html
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Contact Email: |
secretariat@vki.ac.be
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Organizer: |
von Karman Institute for Fluid Dynamics
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Application Areas: |
Turbomachinery
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Special Fields: |
Turbulence Modeling, Turbulence Theory
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Type of Event: |
Conference, International
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Description: |
The present multidisciplinary Lecture Series addresses the
current state of the art in the design and analysis of
axial Turbomachinery components. The course is aimed at
Turbomachinery designers, as well as experimental and CFD
aero-thermal scientists. Both aerodynamic, heat transfer
and mechanical concepts are developed by authors coming
from industry, governmental and research agencies and
universities.
An introductory lecture will discuss the current trends in
engine research. The next course will explain the
successive steps of the aero-design of high-pressure
turbines. Future improvements in the performance of
turbine based propulsion largely depend on our
understanding of unsteady flows. In view of decreasing
weight and costs, current turbomachinery designs tend to
increase the stage loading and to shorten the distance
between blade rows. Several consecutive courses are
dedicated to unsteady effects in HP turbines, LP turbines
and compressors. Sessions on forced response address the
impact of the excitation on blade and disk vibrations.
Current practice of aeromechanical design are presented
and illustrated with practical examples in compressors and
turbines.
Cooling techniques are crucial to guarantee the life of
the HP blades. A special note will address general design
issues and types of calculations used in cooling channels.
Turbine tip clearance improvement, in spite of known
challenges, continues to present one of the most powerful
means for enhancement of gas turbine engine performance.
The experimental and numerical study of various tip
configurations will be addressed as well. Emphasis will
then be put on tip heat transfer and cooling, looking
among other subjects to design aspects and methodologies.
Finally specific lectures will be given on advanced
numerical methods using Large Eddy Simulations.
Afterwards, applications to control the flow in turbines
will be presented.
The current course is an update of previously delivered
courses at the von Karman Institute. The directors of this
course are Prof. Guillermo Paniagua of the von Karman
Institute, and Dr. Richard B. Rivir, of the Wright
Patterson AFB.
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Event record first posted on November 4, 2006, last modified on November 8, 2006
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