A Methodology for Capturing the Impacts of Bleed Flow Extraction on Compressor Performance and Operability in Engine Conceptual Design

نویسنده

  • Jeff Schutte
چکیده

DEDICATION I would like to dedicate this thesis and all of the work herein to my family, my soon to be bride, Jessica, my two loving sisters, Ashley and Amy, and my incredible parents, Robert and Katherine, who have provided me with consistent encouragement and unconditional support throughout the duration of this endeavor. who selflessly provided for me in care, fellowship, support, guidance, friendship, and above all else, love. Love like this can only come from one place, which leads me to my most important dedication of all. It brings me the greatest joy to dedicate, and fully credit this work to my Lord and Savior, Jesus Christ. " Whatever you do, do your work heartily, as for the Lord rather than for men…it is the Lord Christ whom you serve " – Colossians 3:23 Through his blessings alone, I was able to attend this institution, and through his blessings alone I was able to produce this work. " But in all these things we overwhelmingly conquer through Him who loved us. For I am convinced that neither death, nor life, nor angels, nor principalities, nor things present, nor things to come, nor powers, nor height, nor depth, nor any other created thing, will be able to separate us from the love of God, which is in Christ Jesus our Lord. " – Romans 8:37-39 iv ACKNOWLEDGEMENTS I would like to thank Dr. Dimitri Mavris for his guidance and support as my committee chairman throughout the course of this work. His provision for this experience, from believing in me enough to bring me into the ASDL, to encouraging me to complete this research, has been a wonderful blessing in my life. serving on my committee, and for their continued encouragement and technical support throughout the completion of this endeavor. I would like to thank my friends at the ASDL, especially Andrew Miller for his technical advice and fellowship in this work. Finally, I would like to thank my many mentors from my undergraduate work until now, who have inspired my research interests and who stand as role models for my technical work. These include, amongst others, Dr.

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Performance Prediction Modeling of Axial-Flow Compressor by Flow Equations

Design models of multi- stage, axial flow compressor are developed for gas turbine engines. Axial flow compressor is one of the most important parts of gas turbine units. Therefore, its design and performance prediction are very important. One-dimensional modeling is a simple, fast and accurate method for performance prediction of any type of compressors with different geometries. In this appro...

متن کامل

Thermodynamic Analysis and Statistical Investigation of Effective Parameters for Gas Turbine Cycle using the Response Surface Methodology

In this paper, the statistical analyses are presented to study the thermal efficiency and power output of gas turbine (GT) power plants. For analyzing gas turbine operation and performance, a novel approach is developed utilizing the response surface methodology (RSM) which is based on the central composite design (CCD) method. An attempt is made to study the effect of some operational factors ...

متن کامل

Effect of aging and manufacturing tolerances on multi-stage transonic axial compressor performance

The Axial compressor is an integrated part of a gas turbine. The central part of compressors is its blades. Blade aerodynamic has a significant effect on compressor performance. Because of the adverse pressure gradient in the compressor, any deviation in the blade profile has a significant influence on the flow field as well as the compressor performance. During the manufacturing and operation ...

متن کامل

Effect of blade profile on the performance characteristics of axial compressor in design condition

The choice of geometrical shape of the blades has a considerable effect on aerodynamic performance and flow characteristics in axial compressors. In this paper, the effects of the blades shape on the aerodynamic design characteristics are investigated based on Streamline Curvature Method (SCM). Initially, the Streamline Curvature Method (SCM) is used for designing a two-stage axial compressor. ...

متن کامل

Experimental study of the effects of repetitive surge condition on turbocharger performance

When the mass flow rate through the compressor is reduced at a constant pressure ratio, mass flow rate will drop to an extent that the complete reversal of flow and surge occurs. Recently many research focuses on turbocharger surge, however, there are not enough investigation on the effect of surge on the performance of the turbocharger. The aim of the paper is to investigate the effect of repe...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2015