An Investigation of the Effects of Nozzle Guide Vane Trailing Edge Cooling on Rotor Heat Transfer in a Transonic Turbine Stage PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download An Investigation of the Effects of Nozzle Guide Vane Trailing Edge Cooling on Rotor Heat Transfer in a Transonic Turbine Stage PDF full book. Access full book title An Investigation of the Effects of Nozzle Guide Vane Trailing Edge Cooling on Rotor Heat Transfer in a Transonic Turbine Stage by Aaron James Gleixner. Download full books in PDF and EPUB format.

An Investigation of the Effects of Nozzle Guide Vane Trailing Edge Cooling on Rotor Heat Transfer in a Transonic Turbine Stage

An Investigation of the Effects of Nozzle Guide Vane Trailing Edge Cooling on Rotor Heat Transfer in a Transonic Turbine Stage PDF Author: Aaron James Gleixner
Publisher:
ISBN:
Category :
Languages : en
Pages : 330

Book Description


An Investigation of the Effects of Nozzle Guide Vane Trailing Edge Cooling on Rotor Heat Transfer in a Transonic Turbine Stage

An Investigation of the Effects of Nozzle Guide Vane Trailing Edge Cooling on Rotor Heat Transfer in a Transonic Turbine Stage PDF Author: Aaron James Gleixner
Publisher:
ISBN:
Category :
Languages : en
Pages : 330

Book Description


Nozzle Guide Vane Shock Wave Propagation and Bifurcation in a Transonic Turbine Rotor

Nozzle Guide Vane Shock Wave Propagation and Bifurcation in a Transonic Turbine Rotor PDF Author: A. B. Johnson
Publisher:
ISBN:
Category : Bifurcation theory
Languages : en
Pages : 0

Book Description
A study of the propagation of a Nozzle Guide Vane (NGV) trailing edge shock wave through a transonic turbine rotor passage is presented. The work was based on experimental tests carried out in the Isentropic Light Piston Tunnel in Oxford University using a rotating bar NGV shock wave simulator, together with schlieren photography and wide band width surface pressure and heat transfer rate measurements. The study identifies a previously unexplained interaction between the incoming wave and the rotor leading edge, which causes the nucleation of a Vortical Bubble. This bubble has been shown to enhance the thermal loading on the early pressure surface of the blade. A method of controlling this bubble and heat loading is also considered. A previously unseen "Lambda" interaction between the shock wave and the rotor pressure surface is also identified.

Masters Theses in the Pure and Applied Sciences

Masters Theses in the Pure and Applied Sciences PDF Author: Wade H. Shafer
Publisher: Springer Science & Business Media
ISBN: 1461524539
Category : Science
Languages : en
Pages : 391

Book Description
Masters Theses in the Pure and Applied Sciences was first conceived, published, and disseminated by the Center for Information and Numerical Data Analysis and Synthesis (CINDAS)* at Purdue University in 1957, starting its coverage of theses with the academic year 1955. Beginning with Volume 13, the printing and dis semination phases of the activity were transferred to University Microfilms/Xerox of Ann Arbor, Michigan, with the though that such an arrangement would be more beneficial to the academic and general scientific and technical community. After five years of this joint undertaking we had concluded that it was in the interest of all concerned if the printing and distribution of the volumes were handled by an international publishing house to assure improved service and broader dissemi nation. Hence, starting with Volume 18, Masters Theses in the Pure and Applied Sciences has been disseminated on a worldwide basis by Plenum Publishing Corporation of New York, and in the same year the coverage was broadened to include Canadian universities. All back issues can also be ordered from Plenum. We have reported in Volume 37 (thesis year 1992) a total of 12,549 thesis titles from 25 Canadian and 153 United States universities. We are sure that this broader base for these titles reported will greatly enhance the value of this impor tant annual reference work. While Volume 37 reports theses submitted in 1992, on occasion, certain uni versities do report theses submitted in previous years but not reported at the time.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892

Book Description


Heat Transfer Due to Unsteady Effects as Investigated in a High-speed, Full-scale, Fully-cooled Turbine Vane and Rotor Stage

Heat Transfer Due to Unsteady Effects as Investigated in a High-speed, Full-scale, Fully-cooled Turbine Vane and Rotor Stage PDF Author: Jonathan R. Mason
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 236

Book Description


Direct and Large-Eddy Simulation X

Direct and Large-Eddy Simulation X PDF Author: Dimokratis G.E. Grigoriadis
Publisher: Springer
ISBN: 3319632124
Category : Technology & Engineering
Languages : en
Pages : 523

Book Description
This book addresses nearly all aspects of the state of the art in LES & DNS of turbulent flows, ranging from flows in biological systems and the environment to external aerodynamics, domestic and centralized energy production, combustion, propulsion as well as applications of industrial interest. Following the advances in increased computational power and efficiency, several contributions are devoted to LES & DNS of challenging applications, mainly in the area of turbomachinery, including flame modeling, combustion processes and aeroacoustics. The book includes work presented at the tenth Workshop on 'Direct and Large-Eddy Simulation' (DLES-10), which was hosted in Cyprus by the University of Cyprus, from May 27 to 29, 2015. The goal of the workshop was to establish a state of the art in DNS, LES and related techniques for the computation and modeling of turbulent and transitional flows. The book is of interest to scientists and engineers, both in the early stages of their career and at a more senior level.

Blade-to-coolant Heat-transfer Results and Operating Data from a Natural-convection Water-cooled Single-stage Turbine

Blade-to-coolant Heat-transfer Results and Operating Data from a Natural-convection Water-cooled Single-stage Turbine PDF Author: Anthony J. Diaguila
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 28

Book Description


ASME Technical Papers

ASME Technical Papers PDF Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 484

Book Description


Effect of Diameter of Closed-end Coolant Passages on Natural-convection Water Cooling of Gas-turbine Blades

Effect of Diameter of Closed-end Coolant Passages on Natural-convection Water Cooling of Gas-turbine Blades PDF Author: Arthur N. Curren
Publisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 42

Book Description
An experimental investigation on a water-cooled gas turbine with blade coolant-passage diameters ranging from 0.100 to 0.500 inch, corresponding to length-to-diameter ratios of 25.5 to 5.1, in various quadrants of the turbine. The investigation was conducted to determine (1) whether coolant-passage length-to-ratio has a significant effect on natural-convection heat-transfer correlation, and (2) whether turbine blade temperatures could be calculated with reasonable accuracy from a theoretical natural-convection heat-transfer correlation.

Proceedings of the ASME Turbo Expo 2002 Presented at the 2002 ASME Turbo Expo, June 3-6, 2002, Amsterdam, the Netherlands

Proceedings of the ASME Turbo Expo 2002 Presented at the 2002 ASME Turbo Expo, June 3-6, 2002, Amsterdam, the Netherlands PDF Author:
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 726

Book Description
Annotation This is Volume 1 of five volumes that comprise the proceedings of the June 2002 conference, sponsored by the International Gas Turbine Institute (IGTI), a technical institute of the American Society of Mechanical Engineers. The purpose of the conference was to facilitate international exchange and development of educational and technical information related to the design, application, manufacture, operation, maintenance, and environmental impact of all types of gas engines. With an emphasis upon the need for more efficient, cleaner, and more reliable gas turbines, the approximately 130 articles cover various technical aspects of aircraft engines; coal, biomass, and alternative fuels; combustion and fuels; education; electric power; and vehicular and small turbomachines. There is no subject index. Annotation c. Book News, Inc., Portland, OR (booknews.com).