Stored arc-heated air - A concept for a high Reynolds number, Mach number 8 to 10, true temperature test facility

1971 ◽  
Author(s):  
W. BOATRIGHT ◽  
W. OLSTAD
Keyword(s):  
Reynolds Number ◽  
Mach Number ◽  
High Reynolds Number ◽  
Test Facility ◽  
True Temperature ◽  
Heated Air ◽  
High Reynolds ◽  
Temperature Test

scholarly journals Aerodynamics and Heat Transfer Investigations on a High Reynolds Number Turbine Cascade

1991 ◽  
Author(s):  
Taher Schobeiri ◽  
Eric McFarland ◽  
Frederick Yeh
Keyword(s):  
Heat Transfer ◽  
Reynolds Number ◽  
High Reynolds Number ◽  
Test Facility ◽  
Experimental Investigations ◽  
Turbine Cascade ◽  
Calculation Methods ◽  
Transfer Coefficients ◽  
Pressure Distributions ◽  
High Reynolds

In this report the results of aerodynamic and heat transfer experimental investigations performed in a high Reynolds number turbine cascade test facility are analyzed. The experimental facility simulates the high Reynolds number flow conditions similar to those encountered in the space shuttle main engine. In order to determine the influence of Reynolds number on aerodynamic and thermal behavior of the blades, heat transfer coefficients were measured at various Reynolds numbers using liquid crystal temperature measurement technique. Potential flow calculation methods were used to predict the cascade pressure distributions. Boundary layer and heat transfer calculation methods were used with these pressure distributions to verify the experimental results.

1226 THE COLAPIPE - A HIGH REYNOLDS NUMBER PIPE TEST FACILITY

2013 ◽  
Vol 2013.4 (0) ◽  
pp. _1226-1_-_1226-6_
Author(s):  
Konig Franziska ◽  
Zanoun El-Sayed ◽  
Jehring Lothar ◽  
Egbers Christoph
Keyword(s):  
Reynolds Number ◽  
High Reynolds Number ◽  
Test Facility ◽  
High Reynolds

scholarly journals Comparison of turbulence profiles in high-Reynolds-number turbulent boundary layers and validation of a predictive model

2017 ◽  
Vol 814 ◽  
Author(s):  
J.-P. Laval ◽  
J. C. Vassilicos ◽  
J.-M. Foucaut ◽  
M. Stanislas
Keyword(s):  
Reynolds Number ◽  
High Reynolds Number ◽  
Salt Lake ◽  
Reynolds Numbers ◽  
Turbulent Pipe Flow ◽  
Test Facility ◽  
Flow Data ◽  
Wide Range ◽  
Layer Flow ◽  
High Reynolds

The modified Townsend–Perry attached-eddy model of Vassilicos et al. (J. Fluid Mech., vol. 774, 2015, pp. 324–341) combines the outer peak/plateau behaviour of root-mean-square streamwise turbulence velocity profiles and the Townsend–Perry log decay of these profiles at higher distances from the wall. This model was validated by these authors for high-Reynolds-number turbulent pipe flow data and is shown here to describe equally well, and with approximately the same parameter values, turbulent boundary layer flow data from four different facilities and a wide range of Reynolds numbers. The model has predictive value as, when extrapolated to the extremely high Reynolds numbers of the SLTEST data obtained at the Great Salt Lake Desert atmospheric test facility, it matches these data quite well.

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