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Secondary Flow And Heat Transfer Control In Gas Turbine Inlet Nozzle Guide Vanes
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Book Synopsis Secondary Flow and Heat Transfer Control in Gas Turbine Inlet Nozzle Guide Vanes by : Steven Wayne Burd
Download or read book Secondary Flow and Heat Transfer Control in Gas Turbine Inlet Nozzle Guide Vanes written by Steven Wayne Burd and published by . This book was released on 1998 with total page 604 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Numerical Modeling of Heat Transfer and Thermal Stresses in Gas Turbine Guide Vanes by : Faisal Rahman
Download or read book Numerical Modeling of Heat Transfer and Thermal Stresses in Gas Turbine Guide Vanes written by Faisal Rahman and published by . This book was released on 2013 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Due to a relative high thermal efficiency, the gas turbine engine has wide ranging applications in various industries today. The aerospace and power generation sectors are probably the best known. One method of increasing the thermal efficiency of a gas turbine engine is to increase the turbine inlet temperature. This increase in temperature will result in an additional thermal load being placed on the turbine blades and in particular the nozzle guide vanes. The higher temperature gradients will increase the thermal stresses. In order to prevent failure of blades due to thermal stresses, it is important to accurately determine the magnitude of the stresses during the design phase of an engine. The accuracy of the thermal stresses mainly depends on two issues. The first is the determination of the heat transfer from the fluid to the blade and then secondly the prediction of the thermal stresses in the blade as a result of the thermal loading. In this study the flow and heat transfer problem is approached through the use of computational fluid dynamics (CFD). The principal focus is to predict the heat transfer and thermal stresses for steady state cases for both cooled and uncooled nozzle guide vanes through numerical modelling techniques. From the literature, two studies have been identified for which experimental data was available. These case studies can therefore be used to evaluate the accuracy of using CFD to simulate the thermal loading on the blades. One study focused only on solving heat transfer whilst the other included thermal stress modelling. The same methodology is then applied to a three-dimensional application in which flow and heat transfer was solved for a nozzle guide vane of a commercial gas turbine engine. The accuracy of results varied with the choice of turbulence model but was, generally within ten percent of experimental data. It was shown that the accurate determination of the heat transfer to the blade is the key element to accurately determine the thermal stresses.
Book Synopsis Measurements in a Gas Turbine First Stage Nozzle Guide Vane Cascade with Film Cooling and Endwall Contouring by : Rohit Anand Oke
Download or read book Measurements in a Gas Turbine First Stage Nozzle Guide Vane Cascade with Film Cooling and Endwall Contouring written by Rohit Anand Oke and published by . This book was released on 2001 with total page 574 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Secondary Flow Decay Downstream of Turbine Inlet Guide Vane with End-wall Contouring by : V. Michelassi
Download or read book Secondary Flow Decay Downstream of Turbine Inlet Guide Vane with End-wall Contouring written by V. Michelassi 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.
Book Synopsis Flow and Heat Transfer in a Turbine Nozzle Guide Vane with Endwall Contouring by : Y.-L. Lin
Download or read book Flow and Heat Transfer in a Turbine Nozzle Guide Vane with Endwall Contouring written by Y.-L. Lin and published by . This book was released on 2000 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Conjugate Flow and Heat Transfer Calculation of a High Pressure Turbine Nozzle Guide Vane by : Dieter Bohn
Download or read book Conjugate Flow and Heat Transfer Calculation of a High Pressure Turbine Nozzle Guide Vane written by Dieter Bohn and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effects of Secondary Flows on the Heat Transfer to Turbine Nozzle Endwall and Rotor Shroud by : Anthony Chibuzo Nebo
Download or read book The Effects of Secondary Flows on the Heat Transfer to Turbine Nozzle Endwall and Rotor Shroud written by Anthony Chibuzo Nebo and published by . This book was released on 1978 with total page 404 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat Transfer in Gas Turbines by : Bengt Sundén
Download or read book Heat Transfer in Gas Turbines written by Bengt Sundén and published by Witpress. This book was released on 2001 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt: This title presents and reflects current active research on various heat transfer topics and related phenomena in gas turbine systems. It begins with a general introduction to gas turbine heat transfer, before moving on to specific areas.
Book Synopsis Conjugate Heat Transfer of an Internally Air-Cooled Nozzle Guide Vane and Shrouds by : L.-Y. Jiang
Download or read book Conjugate Heat Transfer of an Internally Air-Cooled Nozzle Guide Vane and Shrouds written by L.-Y. Jiang and published by . This book was released on 2018 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: The accurate evaluation of the aero-thermodynamic working environments of gas turbine critical components is essential in the development of advanced gas turbine engines, such as cooling flow arrangement and service life assessment. In this chapter, as a technology demonstration, the conjugate heat transfers of the internally air-cooled nozzle guide vane (NGV) and shrouds of a gas turbine engine at flight conditions are numerically examined. The simulations are performed with a high-fidelity CFD model and adequately defined boundary conditions. The effect of the non-dimensional distance from wall surfaces, y+, on the wall temperature is studied. The characteristics of the complex three-dimensional flow and temperature fields are revealed, and the heat fluxes between the hot gas, NGV body, and cooling airflow at selected cross sections are presented and discussed. It is clear that the traditional one-dimensional semiempirical approach is no longer suitable. Generally, the Mach number is higher, and the temperature is lower on the NGV suction side than on the pressure side. It is found that two high-temperature zones occur on the NGV pressure side and the temperature over the middle section is relatively low. These findings are related to where the cooling holes and outlets are located and consistent with the field observation of NGV damages.
Book Synopsis Numerical and Experimental Investigations of Design Parameters Defining Gas Turbine Nozzle Guide Vane Endwall Heat Transfer by : Frank G. Rubensdörffer
Download or read book Numerical and Experimental Investigations of Design Parameters Defining Gas Turbine Nozzle Guide Vane Endwall Heat Transfer written by Frank G. Rubensdörffer and published by . This book was released on 2006 with total page 138 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 3-D Conjugate Flow and Heat Transfer Calculations of a Film-cooled Turbine Guide Vane at Different Operation Conditions by : Dieter E. Bohn
Download or read book 3-D Conjugate Flow and Heat Transfer Calculations of a Film-cooled Turbine Guide Vane at Different Operation Conditions written by Dieter E. Bohn and published by . This book was released on 1997 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Orlando, FL, Jun 2-Jun 5, 1997.
Book Synopsis Optimization of a Low Heat Load Turbine Nozzle Guide Vane by : Jamie J. Johnson
Download or read book Optimization of a Low Heat Load Turbine Nozzle Guide Vane written by Jamie J. Johnson and published by . This book was released on 2006 with total page 404 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book ASME Technical Papers written by and published by . This book was released on 2000 with total page 574 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flow Behavior in Inlet Guide Vanes of Radial Turbines by :
Download or read book Flow Behavior in Inlet Guide Vanes of Radial Turbines written by and published by . This book was released on 1975 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Conjugate 3-D Flow and Heat Transfer Analysis of a Thermal Barrier Cooled Turbine Guide Vane by : Dieter E. Bohn
Download or read book A Conjugate 3-D Flow and Heat Transfer Analysis of a Thermal Barrier Cooled Turbine Guide Vane written by Dieter E. Bohn 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.
Book Synopsis Secondary Flows in Turbomachines by :
Download or read book Secondary Flows in Turbomachines written by and published by . This book was released on 1990 with total page 341 pages. Available in PDF, EPUB and Kindle. Book excerpt: These proceedings contain the 24 papers presented at the meeting on secondary flows in turbomachines. The meeting was arranged in the following sessions: Basic flow phenomena (6); Experimental results (5); Three-dimensional computation and comparison with experiments (5); Tip clearance flows (4); and Secondary flow effects on heat transfer (4). The specialists' meeting offered a forum for experts to discuss computational and experimental methods and results for secondary flow in cascades, compressors and turbines. CFD was found to be an adequate tool to represent qualitative phenomena, but on the accuracy of predicting losses and exit angles there was some disagreement. Many papers dealt with experimental investigations which are obviously essential for evaluating secondary flow models. Keywords: Three dimensional flow computations; Cascade structures; Axial flow compressors; Airfoils; Turbulent flow/mixing; Nozzle guide vanes; Transonic nozzles; Aspect ratio; Centrifugal impellers; Radial compressors; Blade tips; Turbine blades; Cascades fluid dynamics; Compressors; End wall flow; Computational fluid dynamics; Tip leakage flow; Secondary flow; Turbine guide vanes.