Author: D. W. LuckeyPublisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 388
Book Description
Stagnation Region Gas Film Cooling
Author: D. W. LuckeyPublisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 388
Book Description
Stagnation Region Gas Film Cooling Spanwise Angled Coolant Injection
Author: David W. LuckeyPublisher:
ISBN:
Category :
Languages : en
Pages : 357
Book Description
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.
Stagnation Region Gas Film Cooling
Author: Edwin R. YarbroughPublisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 0
Book Description
Stagnation Region Gas Film Cooling
Author: David Wilson LuckeyEffect on Gaseous Film Cooling of Coolant Injection Through Angled Slots and Normal Holes
Author: S. Stephen PapellPublisher:
ISBN:
Category : Cooling
Languages : en
Pages : 32
Book Description
Stagnation Region Gas Film Coding
Author: D. W. LuckeyPublisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 372
Book Description
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 784
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Proceedings Of The International Heat Transfer Conference
Author: LeePublisher: CRC Press
ISBN: 9781560327974
Category : Science
Languages : en
Pages : 696
Book Description
This year's set of papers includes 23 Keynote Papers and 537 refereed General Papers, in seven volumes. Experts from around the world have combined to address the leading edge of research and practical innovations in convection, combustion, heat exchangers, two-phase flow, and much more. Whether one is involved in mechanical, chemical, nuclear, or energy engineering the quantity, international scope, and high quality of the contents make access to these volumes essential.
Full-coverage Film Cooling on Flat, Isothermal Surfaces: Data and Predictions
Author: Flow visualization of film cooling with spanwise injection from a small array of holes and compound-angle injection from a large array
Author: Louis M. RussellPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 24
Book Description