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Turbulent-heat-transfer measurements at a Mach number of 2.06

Description: Report presenting turbulent-heat-transfer measurements obtained through the use of an axially symmetric annual nozzle consisting of an inner shaped center body and an outer cylindrical sleeve at Mach number 2.06. Results regarding the variation of wall temperature with longitudinal distance, variation of local Nusselt number with local Reynolds number, and variation of local temperature-recovery factor with local Reynolds number are provided.
Date: March 1955
Creator: Brevoort, Maurice J. & Rashis, Bernard
Partner: UNT Libraries Government Documents Department
open access

Summary of experimental heat-transfer measurements in turbulent flow for a Mach number range from 0.87 to 5.05

Description: Report presenting heat-transfer measurements made in turbulent flow at a variety of Mach and Reynolds numbers through the use of an axially symmetric annular nozzle consisting of an inner shaped center body and an outer cylindrical sleeve. The results are presented as Stanton number and recovery factor as a function of Reynolds number. Stanton number was found to decrease with an increase in Reynolds number and usually decreases with an increase in Mach number.
Date: May 1958
Creator: Brevoort, Maurice J. & Arabian, Barbara D.
Partner: UNT Libraries Government Documents Department
open access

Turbulent-heat-transfer measurements at a Mach number of 0.87

Description: Report presenting turbulent-heat-transfer measurements obtained through the use of an axially symmetric annular nozzle consisting of an inner shaped center body and an outer cylindrical sleeve. Results regarding the wall temperatures, variation of local Nusselt number with Reynolds number, density, velocity, and local temperature-recovery factor are provided.
Date: December 1955
Creator: Brevoort, Maurice J. & Rashis, Bernard
Partner: UNT Libraries Government Documents Department
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