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Books Results
Source: The Open Library
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1Effect of coolant temperature and mass flow on film cooling of turbine blades
By Vijay Kumar Garg
“Effect of coolant temperature and mass flow on film cooling of turbine blades” Metadata:
- Title: ➤ Effect of coolant temperature and mass flow on film cooling of turbine blades
- Author: Vijay Kumar Garg
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Effect of coolant temperature and mass flow on film cooling of turbine blades” Subjects and Themes:
- Subjects: ➤ Stagnation temperature - Stagnation pressure - Hole distribution (Mechanics) - Rotors - Compressibility - Turbine blades - Film cooling
Edition Identifiers:
- The Open Library ID: OL15497736M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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Wiki
Source: Wikipedia
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Stagnation temperature
thermodynamics and fluid mechanics, stagnation temperature is the temperature at a stagnation point in a fluid flow. At a stagnation point, the speed of the fluid
Temperature
of temperature – Method to measure temperature quantitatively Sea surface temperature – Water temperature close to the ocean's surface Stagnation temperature –
Stagnation pressure
flow, the stagnation enthalpy or stagnation temperature plays a role similar to the stagnation pressure in incompressible flow. Stagnation pressure is
Solar thermal collector
the melting point of polypropylene is 160 °C (320 °F), while the stagnation temperature of insulated thermal collectors can exceed 180 °C (356 °F) if control
Kiel probe
A Kiel probe is a device for measuring stagnation pressure or stagnation temperature in fluid dynamics. It is a variation of a Pitot probe where the inlet
Afterburner
entry) temperature, resulting in a significant increase in engine thrust. In addition to the increase in afterburner exit stagnation temperature, there
Rayleigh flow
temperature, velocity and stagnation pressure are shown below, respectively. They are represented graphically along with the stagnation temperature ratio
Total air temperature
In aviation, stagnation temperature is known as total air temperature and is measured by a temperature probe mounted on the surface of the aircraft. The
Compressible flow
steady, and adiabatic flow of a perfect gas is assumed. Stagnation temperature and stagnation enthalpy are the same upstream and downstream of the shock
Hypersonic speed
total enthalpy (MJ/kg), total pressure (kPa-MPa), stagnation pressure (kPa-MPa), stagnation temperature (K), or flow velocity (km/s).[citation needed] Wallace