Measurements in Film Cooling Flows with Lateral Injection A THESIS SUBMITTED TO THE FACULTY OF THE GRADUATE SCHOOL OF THE UNIVERSITY OF MINNESOTA BY Richard W. Kaszeta IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE

نویسنده

  • Terrence W. Simon
چکیده

Measurements of mean velocity, turbulence intensity, and turbulent shear stresses are presented for the mixing region of a film cooling situation in which the coolant is laterally injected. Measurements are performed using triple-wire anemometry so that all three mean velocity components are documented. Such measurements also give Reynolds stress terms in the flow field. Flow with one row of film cooling holes inclined 35◦ to the surface, with lateral injection (Φ = 90◦), is documented. The freestream turbulence intensity level is 12%, and coolant-to-mainstream velocity ratios are 0.5 and 1.0 (the density ratio is unity). General flow field characteristics are discussed and compared. Additional comparisons are made with similar measurements in a flow in which the injection is streamwise (Φ = 0◦).

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

Thesis Submitted in Partial Fulfillment of the requirement for the Degree of M.A/M. Sc In School consultant

Goal: The aim of this study is assess and compare emotional ability of deaf. Semi _ deaf and hearing students (14 _ 20) in Mashhad. Method: To do this experiment out of studies evidence   generally 105 students selecting randomly. From each group, choose the number of normal boys and girls 35, deaf boys and girls and semi deaf boys and girls .this article is useful and explanatory .in this stud...

متن کامل

A Turán Theorem for Random Graphs Dean of the Graduate School Date a Turán Theorem for Random Graphs a Turán Theorem for Random Graphs

of a thesis submitted to the Faculty of the Graduate School of Emory University in partial fulfillment of the requirements of the degree of Master of Science Department of Mathematics and Computer Science

متن کامل

Numerical Simulation Of the Componend Angles Effects On Adiabatic Film Cooling Effectiveness

Abstract Film Cooling Adiabatic Effectiveness on a Profile of a Gas Turbine blade that Using Holes with 45 Degree Combined Angles to the Flow Direction and Radial Along the Attack Edge as well as 25 Degree Angles to the Flow Direction and Surface Area of the Attack Edge Area and 35 degrees relative to the outlet hole suefaces along stagnation line, Under a specified blowing ratios, using the Re...

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 1998