Download or read book Experimental and Numerical Investigation of Turbine Cascade Flow written by V. Michelassi and published by . This book was released on 1992 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental and Numerical Investigation of Transonic Turbine Cascade Flow written by Tibor Kiss and published by . This book was released on 1992 with total page 582 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental and Numerical Investigation of Boundary layer and Wake Development in a Transonic Turbine Cascade written by Vittorio Michelassi and published by . This book was released on 1998 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental and Numerical Investigation of Time Varying Wakes Behind Turbine Blades written by and published by Friedr Vieweg & Sohn Verlagsgesellschaft. This book was released on 1999 with total page 268 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental and Numerical Study of Transonic Turbine Cascade Flow written by Tibor Kiss and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental Investigation of Loss in an Annular Cascade of Turbine nozzle Blades of Free Vortex Design written by Hubert W. Allen and published by . This book was released on 1953 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of the flow pattern immediately downstream of an annular cascade of nozzle blades designed for vortex-type velocity distribution and hub discharge angle of approximately 65 degrees from axial was conducted in order to obtain a better understanding of the processes by which the distribution of losses and deviations from design turning angle occur. For the two Mach numbers investigated, the loass region at the outer shroud decreased while that at the inner shroud increased with increasing Mach number.

Download or read book Numerical and experimental investigation of the wake flow downstream of a linear turbine cascade ASME 98 GT 246 written by Wolfgang Sanz and published by . This book was released on 1998 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm, Sweden, June 2 - June 5, 1998.

Download or read book Analysis of two dimensional turbine cascade flow by finite area method written by and published by . This book was released on 1985 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Experimental and Numerical Investigation of the Flow Field in the Turbine Stator of a Variable Geometry Turbocharger written by J. W. O'Neill and published by . This book was released on 2004 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental and Numerical Investigation of Axial Turbine Models written by Berhanu Mulu Geberkiden and published by . This book was released on 2009 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Numerical Investigation of Time Resolved Flows Around Turbine Blades written by Edward J. Brooksbank and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental and Computational Investigation of Flow Through an Annular Turbine Cascade written by William Howard Donovan and published by . This book was released on 1995 with total page 81 pages. Available in PDF, EPUB and Kindle. Book excerpt: The purpose of this research was to compare numerical predictions with experimental results and to devise an accurate laser anemometry technique to measure in the endwall region of a confined annulus. Flowfield characteristics were computed using a three-dimensional flow solver with the numerical plane coincident with the experimental measurement location. An annular turbine cascade, designed for laser-Doppler velocimetry, was modified to obtain blade passage midspan surface pressure measurements. A range of predicted subsonic and transonic midspan surface pressures were compared favorably with experimental measurements. Two-dimensional Mach number, flow angle, and turbulence intensity measurements were obtained with a fiber-optics laser- Doppler velocimeter. These measurements were performed through a 1.0922 millimeter opening in the endwall at depths ranging from 0.01 mm to 3.34 mm and the results were compared with numerical predictions. (AN).

Download or read book Experimental investigation of the flow field downstream of a plane turbine cascade in transonic flow written by R. Kiock and published by . This book was released on 1977 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental and Computational Investigation of Flow Through an Annular Turbine Cascade written by and published by . This book was released on 1995 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: The purpose of this research was to compare numerical predictions with experimental results and to devise an accurate laser anemometry technique to measure in the endwall region of a confined annulus. Flowfield characteristics were computed using a three-dimensional flow solver with the numerical plane coincident with the experimental measurement location. An annular turbine cascade, designed for laser-Doppler velocimetry, was modified to obtain blade passage midspan surface pressure measurements. A range of predicted subsonic and transonic midspan surface pressures were compared favorably with experimental measurements. Two-dimensional Mach number, flow angle, and turbulence intensity measurements were obtained with a fiber-optics laser-Doppler velocimeter. These measurements were performed through a 1.0922 millimeter opening in the endwall at depths ranging from 0.01 mm to 3.34 mm and the results were compared with numerical predictions. (AN).

Download or read book Experimental Investigation of Heat Transfer in Separated Flow on a Highly Loaded LP Turbine Cascade written by and published by . This book was released on 2003 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Today aerodynamic design tools and CFD-codes provide excellent quality in predicting 2D and 3D flows in turbine components. Nevertheless correlation and numerical methods are not able to predict beat flux in a satisfactory accuracy for complex heat transfer problems for example 3D film cooling mixing zones or areas of separated flow. In order to close part of these gaps in knowledge and to improve the understanding of the interaction between the flow pattern and the beat transfer phenomena experimental investigations were carried out focused on 2D separated flow on the pressure side leading edge of the highly loaded low pressure turbine cascade named T106-300. The cascade was instrumented with pressure taps and glue-on hot-film sensors. The pressure taps provided the static profile pressure distribution. The hot-film anemometry technique normally is used to detect boundary layer development; moreover a procedure will be presented to evaluate the heat transfer coefficient as well. Supplementary boundary layer traverses with a 1D hot-wire probe were carried out at positions inside and downstream of the separation. The dimension of the separation tip to 60% chord was varied by the incidence angle. By variation of Reynolds number and Mach number a data set is available which will be put down to a correlation.

Download or read book Gas Turbine Heat Transfer and Cooling Technology Second Edition written by Je-Chin Han and published by CRC Press. This book was released on 2012-11-27 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt: A comprehensive reference for engineers and researchers, Gas Turbine Heat Transfer and Cooling Technology, Second Edition has been completely revised and updated to reflect advances in the field made during the past ten years. The second edition retains the format that made the first edition so popular and adds new information mainly based on selected published papers in the open literature. See What’s New in the Second Edition: State-of-the-art cooling technologies such as advanced turbine blade film cooling and internal cooling Modern experimental methods for gas turbine heat transfer and cooling research Advanced computational models for gas turbine heat transfer and cooling performance predictions Suggestions for future research in this critical technology The book discusses the need for turbine cooling, gas turbine heat-transfer problems, and cooling methodology and covers turbine rotor and stator heat-transfer issues, including endwall and blade tip regions under engine conditions, as well as under simulated engine conditions. It then examines turbine rotor and stator blade film cooling and discusses the unsteady high free-stream turbulence effect on simulated cascade airfoils. From here, the book explores impingement cooling, rib-turbulent cooling, pin-fin cooling, and compound and new cooling techniques. It also highlights the effect of rotation on rotor coolant passage heat transfer. Coverage of experimental methods includes heat-transfer and mass-transfer techniques, liquid crystal thermography, optical techniques, as well as flow and thermal measurement techniques. The book concludes with discussions of governing equations and turbulence models and their applications for predicting turbine blade heat transfer and film cooling, and turbine blade internal cooling.

Download or read book A Numerical and Experimental Investigation of Turbine Tip Gap Flow written by G. Chen and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: