NASA Technical Reports Server (NTRS) 19890004385: The Effects Of Inlet Turbulence And Rotor/stator Interactions On The Aerodynamics And Heat Transfer Of A Large-scale Rotating Turbine Model, Volume 1 - Info and Reading Options
By NASA Technical Reports Server (NTRS)
"NASA Technical Reports Server (NTRS) 19890004385: The Effects Of Inlet Turbulence And Rotor/stator Interactions On The Aerodynamics And Heat Transfer Of A Large-scale Rotating Turbine Model, Volume 1" and the language of the book is English.
“NASA Technical Reports Server (NTRS) 19890004385: The Effects Of Inlet Turbulence And Rotor/stator Interactions On The Aerodynamics And Heat Transfer Of A Large-scale Rotating Turbine Model, Volume 1” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19890004385: The Effects Of Inlet Turbulence And Rotor/stator Interactions On The Aerodynamics And Heat Transfer Of A Large-scale Rotating Turbine Model, Volume 1
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19890004385
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"NASA Technical Reports Server (NTRS) 19890004385: The Effects Of Inlet Turbulence And Rotor/stator Interactions On The Aerodynamics And Heat Transfer Of A Large-scale Rotating Turbine Model, Volume 1" Description:
The Internet Archive:
A combined experimental and analytical program was conducted to examine the effects of inlet turbulence on airfoil heat transfer. Heat transfer measurements were obtained using low conductivity airfoils with miniature thermocouples welded to a thin, electrically heated surface skin. Heat transfer data were acquired for various combinations of low or high inlet turbulence intensity, flow coefficient (incidence), first-stator/rotor axial spacing, Reynolds number, and relative circumferential position of the first and second stators. Aerodynamic measurements include distributions of the mean and fluctuating velocities at the turbine inlet and, for each airfoil row, midspan airfoil surface pressures and circumferential distributions of the downstream steady state pressures and fluctuating velocities. Analytical results include airfoil heat transfer predictions and a examination of solutions of the unstead boundary layer equipment.
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