Author: Pratik Santosh BhansaliPublisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Jet Impingement Heat Transfer Over Rotating Surfaces
Author: Pratik Santosh BhansaliPublisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Impingement Jet Cooling in Gas Turbines
Author: R.S. AmanoPublisher: WIT Press
ISBN: 1845649060
Category : Science
Languages : en
Pages : 253
Book Description
Due to the requirement for enhanced cooling technologies on modern gas turbine engines, advanced research and development has had to take place in field of thermal engineering. Among the gas turbine cooling technologies, impingement jet cooling is one of the most effective in terms of cooling effectiveness, manufacturability and cost. The chapters contained in this book describe research on state-of-the-art and advanced cooling technologies that have been developed, or that are being researched, with a variety of approaches from theoretical, experimental, and CFD studies. The authors of the chapters have been selected from some of the most active researchers and scientists on the subject. This is the first to book published on the topics of gas turbines and heat transfer to focus on impingement cooling alone.
Single and Multiple Jet Impingement Heat Transfer on Rotating Disks
Author: D. MetzgerMultiple Jet Impingement Heat Transfer Characteristic
Author: Jet Impingement Heat Transfer in Various Cooling Configurations Under Stationary and Rotating Conditions
Author: Srivatsan MadhavanAn Experimental Study of Local Heat Transfer to an Impinging Jet on Non-flat Surfaces
Author: Masood MesbahJet Impingement Heat Transfer in Two-pass Rotating Rectangular Channels
Author: Yuming ZhangHeat Transfer on a Rotating Disk with Single, Axisymmetric Jet Impingement Cooling
Author: Robert William HenryPublisher:
ISBN:
Category : Disks, Rotating
Languages : en
Pages : 324
Book Description
Three-Dimensional Attached Viscous Flow
Author: Ernst Heinrich HirschelPublisher: Springer Science & Business Media
ISBN: 3642413781
Category : Technology & Engineering
Languages : en
Pages : 396
Book Description
Viscous flow is treated usually in the frame of boundary-layer theory and as two-dimensional flow. Books on boundary layers give at most the describing equations for three-dimensional boundary layers, and solutions often only for some special cases. This book provides basic principles and theoretical foundations regarding three-dimensional attached viscous flow. Emphasis is put on general three-dimensional attached viscous flows and not on three-dimensional boundary layers. This wider scope is necessary in view of the theoretical and practical problems to be mastered in practice. The topics are weak, strong, and global interaction, the locality principle, properties of three-dimensional viscous flow, thermal surface effects, characteristic properties, wall compatibility conditions, connections between inviscid and viscous flow, flow topology, quasi-one- and two-dimensional flows, laminar-turbulent transition and turbulence. Though the primary flight speed range is that of civil air transport vehicles, flows past other flying vehicles up to hypersonic speeds are also considered. Emphasis is put on general three-dimensional attached viscous flows and not on three-dimensional boundary layers, as this wider scope is necessary in view of the theoretical and practical problems that have to be overcome in practice. The specific topics covered include weak, strong, and global interaction; the locality principle; properties of three-dimensional viscous flows; thermal surface effects; characteristic properties; wall compatibility conditions; connections between inviscid and viscous flows; flow topology; quasi-one- and two-dimensional flows; laminar-turbulent transition; and turbulence. Detailed discussions of examples illustrate these topics and the relevant phenomena encountered in three-dimensional viscous flows. The full governing equations, reference-temperature relations for qualitative considerations and estimations of flow properties, and coordinates for fuselages and wings are also provided. Sample problems with solutions allow readers to test their understanding.
Author: Gerhard Bosch