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Author : D. W. Luckey
Publisher :
ISBN 13 :
Total Pages : 388 pages
Book Rating : 4.:/5 (31 download)
Download or read book Stagnation Region Gas Film Cooling written by D. W. Luckey and published by . This book was released on 1981 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Edwin R. Yarbrough
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (141 download)
Download or read book Stagnation Region Gas Film Cooling written by Edwin R. Yarbrough and published by . This book was released on 1978 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Byron L. Swenson
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)
Download or read book An Approximate Analysis of Film Cooling on Blunt Bodies by Gas Injection Near the Stagnation Point written by Byron L. Swenson and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Warren J. Mick
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (115 download)
Download or read book An Experimental Study of Stagnation Region Film Cooling for Application to Gas Turbine Airfoils written by Warren J. Mick and published by . This book was released on 1983 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : David W. Luckey
Publisher :
ISBN 13 :
Total Pages : 357 pages
Book Rating : 4.:/5 (227 download)
Download or read book Stagnation Region Gas Film Cooling Spanwise Angled Coolant Injection written by David W. Luckey and published by . This book was released on 1976 with total page 357 pages. Available in PDF, EPUB and Kindle. Book excerpt: This experimental investigation involved the study of gas film cooling from a single row of spanwise angled holes using the stagnation region of a cylinder in cross flow to model the leading edge of a turbine vane. The objective was to obtain data for the local convective heat transfer rates to a highly cooled, curved surface exposed to a turbulent hot mainstream flow and a secondary, film coolant flow. Since the leading edge of the first stage, inlet turbine vane experiences some of the most severe thermal loads found in the turbine engine, effective film cooling is most important in this area. Film cooling of the leading edge area was modeled by making heat transfer measurements on the front stagnation region of a cylinder in cross flow. Experiments were conducted in a rectangular duct using a film cooled cylindrical test surface normal to a two-dimensional freestream flow. A gas turbine combustor provided heated air flow to simulate a Reynolds number typical of a high pressure, high temperature turbine vane. Internal convection cooling of the cylinder allowed a gas-to-wall temperature ratio of 2.1 to be achieved while using a moderate freestream gas temperature (1000R; 555K. The film coolant was chilled to obtain a coolant-to-freestream density ratio of 2.2, representative of the gas turbine environment. The cylindrical test surface was instrumented with miniature heat flux gages, and wall thermocouples to determine the influence of the film coolant blowing ratio and the injection hole geometry on the film cooling performance.
Author : David Wilson Luckey
Publisher :
ISBN 13 :
Total Pages : 372 pages
Book Rating : 4.:/5 (25 download)
Download or read book Stagnation Region Gas Film Cooling written by David Wilson Luckey and published by . This book was released on 1981 with total page 372 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Byron L. Swenson
Publisher : BiblioGov
ISBN 13 : 9781289269203
Total Pages : 44 pages
Book Rating : 4.2/5 (692 download)
Download or read book An Approximate Analysis of Film Cooling on Blunt Bodies by Gas Injection Near the Stagnation Point written by Byron L. Swenson and published by BiblioGov. This book was released on 2013-08 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate method for the estimation of laminar heat transfer to blunt bodies with gaseous film cooling i s developed. Attention is focused on the parameters which are important for the design of an attractive heat protection system. Application of the analysis is made to calculate the approximate coolant weight requirement for both a circular and a parabolic entry.
Author : Ernst Rudolf Georg Eckert
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.3/5 (126 download)
Download or read book Survey of Advantages and Problems Associated with Transpiration Cooling and Film Cooling of Gas-turbine Blades written by Ernst Rudolf Georg Eckert and published by . This book was released on 1951 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: Transpiration and film cooling promise to be effective methods of cooling gas-turbine blades; consequently, analytical and experimental investigations are being conducted to obtain a better understanding of these processes. This report serves as an introduction to these cooling methods, explains the physical processes, and surveys the information available for predicting blade temperatures and heat-transfer rates. In addition, the difficulties encountered in obtaining a uniform blade temperature are discussed, and the possibilities of correcting these difficulties are indicated. Air is the only coolant considered in the application of these cooling methods.
Author : Leonard Roberts
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (31 download)
Download or read book Mass Transfer Cooling Near the Stagnation Point written by Leonard Roberts and published by . This book was released on 1959 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: A simplified analysis is made of mass transfer cooling--that is, injection of a foreign gas--near the stagnation point for two-dimensional and axisymmetric bodies. The reduction in heat transfer is given in terms of the properties of the coolant gas and it is shown that the heat transfer may be reduced considerably by the introduction of a gas having appropriate thermal and diffusive properties. The mechanism by which heat transfer is reduced is discussed.
Author : Byron L. Swenson
Publisher :
ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)
Download or read book An Approximate Analysis of Film Cooling on Blunt Bodies by Gas Injection Near the Stagnation Point written by Byron L. Swenson and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate method for the estimation of laminar heat transfer to blunt bodies with gaseous film cooling is developed. Attention is focused on the parameters which are important for the design of an attractive heat protection system. Application of the analysis is made to calculate the approximate coolant weight requirement for both a circular and a parabolic entry. (Author).
Author : Virginia C. Witteveld
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (137 download)
Download or read book Film cooling effectiveness in the showerhead region of a gas turbine vane Part II: Stagnation region and near-suction side, ASME 99-GT-49 written by Virginia C. Witteveld and published by . This book was released on 1999 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Indianapolis, Indiana, June 7-June 10, 1999.
Author : Marc D. Polanka
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (137 download)
Download or read book Film cooling effectiveness in the showerhead region of a gas turbine vane Part I: Stagnation region and near-pressure side, ASME 99-GT-48 written by Marc D. Polanka and published by . This book was released on 1999 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Indianapolis, Indiana, June 7-June 10, 1999.
Author : Cheryl A. Martin
Publisher :
ISBN 13 :
Total Pages : 442 pages
Book Rating : 4.:/5 (89 download)
Download or read book Numerical Simulations of Leading Edge Film Cooling Flows for Gas Tubine Airfoils written by Cheryl A. Martin and published by . This book was released on 1997 with total page 442 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 14 pages
Book Rating : 4.:/5 (494 download)
Download or read book Dossier Ushio Amagatsu written by and published by . This book was released on 1991 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Robert E. Dannenberg
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (31 download)
Download or read book Helium Film Cooling on a Hemisphere at a Mach Number of 10 written by Robert E. Dannenberg and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John E. Grimaud
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (31 download)
Download or read book Experimental Data on Stagnation-point Gas Injection Cooling on a Hemisphere-cone in a Hypersonic Arc Tunnel written by John E. Grimaud and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Je-Chin Han
Publisher : CRC Press
ISBN 13 : 9781560328414
Total Pages : 666 pages
Book Rating : 4.3/5 (284 download)
Download or read book Gas Turbine Heat Transfer and Cooling Technology written by Je-Chin Han and published by CRC Press. This book was released on 2001-03-22 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is intended to be a reference book for engineers working and interested in gas turbine heat transfer analysis and cooling design for advanced research. The methods presented in this book can be applied to heat exchangers, nuclear power plants and electronic component cooling.
