Author: Peitong JinPublisher:
ISBN:
Category :
Languages : en
Pages : 600
Book Description
Local Measurement and Numerical Modeling of Mass/heat Transfer from a Turbine Blade in a Linear Cascade with Tip Clearance
Author: Peitong JinNumerical Simulations on Flow and Heat Transfer in Turbine Cascade and Tip Clearance Over Shrouded Blades
Author: Yumin XiaoPublisher:
ISBN:
Category : Cascades (Fluid dynamics)
Languages : en
Pages : 236
Book Description
Proceedings of the ASME Turbo Expo 2002
Author: Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 590
Book Description
Annotation Volumes 3A and 3B are part of a five-volume set comprising the proceedings of the June 2002 conference held in the Netherlands. Approximately 125 articles address heat transfer, and manufacturing materials and metallurgy. A sampling of topics: the effect of freestream turbulence on film cooling adiabatic effectiveness; the influence of periodic unsteady inflow conditions on leading edge film cooling; and fluid dynamcis of a pre-swirl rotor-stator system. No subject index. Annotation c. Book News, Inc., Portland, OR (booknews.com).
The Heat and Mass Transfer Analogy Factor, Nu/Sh for 2-D and 3-D Boundary Layers
Author: Sangjo HanAmerican Doctoral Dissertations
Author: Publisher:
ISBN:
Category : Dissertation abstracts
Languages : en
Pages : 816
Book Description
Endwall Heat Transfer Measurements in a Transonic Turbine Cascade
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Turbine blade endwall heat transfer measurements are given for a range of Reynolds and Mach numbers. Data were obtained for Reynolds numbers based on inlet conditions of 0.5 and 1.0 x 10(exp 6), for isentropic exit Mach numbers of 1.0 and 1.3, and for freestream turbulence intensities of 0.25% and 7.0%. Tests were conducted in a linear cascade at the NASA Lewis Transonic Turbine Blade Cascade Facility. The test article was a turbine rotor with 136 deg of turning and an axial chord of 12.7 cm. The large scale allowed for very detailed measurements of both flow field and surface phenomena. The intent of the work is to provide benchmark quality data for CFD code and model verification. The flow field in the cascade is highly three-dimensional as a result of thick boundary layers at the test section inlet. Endwall heat transfer data were obtained using a steady-state liquid crystal technique.
Local Mass Transfer Measurement from a Turbine Blade
Author: Haiping WangDissertation Abstracts International
Author: Publisher:
ISBN:
Category : Dissertations, Academic
Languages : en
Pages : 832
Book Description
Paper
Author: Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 434
Book Description
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 488
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.