Author: United States. Congress. House. Committee on Appropriations. Subcommittee on VA, HUD, and Independent AgenciesPublisher:
ISBN:
Category : United States
Languages : en
Pages : 816
Book Description
Departments of Veterans Affairs and Housing and Urban Development, and Independent Agencies Appropriations for 1995
Author: United States. Congress. House. Committee on Appropriations. Subcommittee on VA, HUD, and Independent AgenciesPublisher:
ISBN:
Category : United States
Languages : en
Pages : 816
Book Description
Springer Handbook of Experimental Fluid Mechanics
Author: Cameron TropeaPublisher: Springer Science & Business Media
ISBN: 3540251413
Category : Science
Languages : en
Pages : 1570
Book Description
Accompanying DVD-ROM contains ... "all chapters of the Springer Handbook."--Page 3 of cover.
Flow and Noise Control: Review and Assessment of Future Directions
Author: Russell H. ThomasPublisher:
ISBN:
Category : Aerodynamical noise
Languages : en
Pages : 98
Book Description
AIAA Journal
Author: American Institute of Aeronautics and AstronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1380
Book Description
AGARD Index of Publications
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and DevelopmentPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 614
Book Description
Measurements of Heat Transfer, Flow, and Pressures in a Simulated Turbine Blade Internal Cooling Passage
Author: Louis M. RussellPublisher:
ISBN:
Category : Flow visualization
Languages : en
Pages : 30
Book Description
An experimental study was made to obtain quantitative information on heat transfer, flow, and pressure distribution in a branched duct test section that had several significant features of an internal cooling passage of a turbine blade. The objective of this study was to generate a set of experimental data that could be used for validation of computer codes that would be used to model internal cooling. Surface heat transfer coefficients and entrance flow conditions were measured at nominal entrance Reynolds numbers of 45 000, 335 000, and 726 000. Heat transfer data were obtained by using a steady-state technique in which an Inconel heater sheet is attached to the surface and coated with liquid crystals. Visual and quantitative flow-field data from particle image velocimetry measurements for a plane at midchannel height for a Reynolds number of 45 000 were also obtained. The flow was seeded with polystyrene particles and illuminated by a laser light sheet. Pressure distribution measurements were made both on the surface with discrete holes and in the flow field with a total pressure probe. The flow-field measurements yielded flow-field velocities at selected locations. A relatively new method, pressure sensitive paint, was also used to measure surface pressure distribution. The pressure paint data obtained at Reynolds numbers of 335 000 and 726 000 compared well with the more standard method of measuring pressures by using discrete holes.
Applied Mechanics Reviews
Author: Pressure and Temperature Sensitive Paints
Author: Tianshu LiuPublisher: Springer Science & Business Media
ISBN: 3540266445
Category : Technology & Engineering
Languages : en
Pages : 331
Book Description
Luminescent molecule sensors, called pressure-sensitive paint (PSP) and temperature-sensitive paint (TSP), measure factors essential for understanding the aerodynamic performance and heat transfer characteristics of flight vehicles. They provide a powerful tool for experimental aerodynamicists to obtain a deeper understanding of the rich physical phenomena in complex flows around a flight vehicle. This book helps the reader to understand the physics and chemistry and the capabilities of PSP and TSP. It provides an overview of the wide scope of applications and explains the system requirements for using these sensors. The book also includes an extensive table of properties of PTP and TSP. As such, it is a thorough and up-to-date coverage of the underlying physics and applications of luminescent molecules designed for global pressure and temperature mapping
Author: 
Author: