Pressure and Heat-transfer Distributions of 0.1-scale Gemini Exit and Reentry Models at Mach Numbers of 3.51 and 4.44
Author:
Publisher:
Published: 1965
Total Pages: 116
ISBN-13:
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Measurements of the Surface Flows, Heat Transfer, Pressure Distribution, and Longitudinal Stability of a Mercury Capsule Model at Mach Numbers of 6.9 and 9.6
Author: Philip E. Everhart
Publisher:
Published: 1961
Total Pages: 66
ISBN-13:
DOWNLOAD EBOOKMeasurements of the Surface Flows, Heat Transfer, Pressure Distribution, and Longitudinal Stability of a Mercury Capsule Model at Mach Numbers of 6.9 and 9.6
Author:
Publisher:
Published: 1961
Total Pages: 62
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DOWNLOAD EBOOKEffects of Mach Number and Wall-temperature Ratio on Turbulent Heat Transfer at Mach Numbers from 3 to 5
Author: Thorval Tendeland
Publisher:
Published: 1959
Total Pages: 28
ISBN-13:
DOWNLOAD EBOOKThe heat-transfer data obtained from the model were found to correlate when the T' method of Sommer and Short was used. The increase in turbulent heat-transfer rate with a reduction in wall to free-stream temperature ratio was of the same order of magnitude as has been found for the turbulent skin-friction coefficient.
Variation in Heat Transfer During Transient Heation of a Hemisphere at a Mach Numer of 2
Author: Roland D. English
Publisher:
Published: 1960
Total Pages: 30
ISBN-13:
DOWNLOAD EBOOKPressure Distribution on Two Models of a Project Mercury Capsule for a Mach Number Range of 1.60 to 6.01 and an Angle-of-attack Range of 0°degress to 180°
Author: Robert A. Newlander
Publisher:
Published: 1960
Total Pages: 102
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DOWNLOAD EBOOKEffect of Shock Impingement on the Heat-transfer and Pressure Distributions on a Cylindrical-leading-edge Model at Mach Number 19
Author: L. G. Siler
Publisher:
Published: 1964
Total Pages: 36
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DOWNLOAD EBOOKHeat-transfer and Pressure Distributions of Two Flat-face Sharp-corner Bodies of Revolution at a Mach Number of 8 and Comparison with Data for a Round-corner Body
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Publisher:
Published: 1963
Total Pages: 36
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DOWNLOAD EBOOKHeat Transfer for Mach Numbers Up to 2.2 and Pressure Distributions for Mach Numbers Up to 4.7 from Flight Investigations of a Flat-face-cone and a Hemisphere-cone
Author: Katherine C. Speegle
Publisher:
Published: 1958
Total Pages: 60
ISBN-13:
DOWNLOAD EBOOKMeasurements of Shock-impingement Effects on the Heat-transfer and Pressure Distributions on a Hemicylinder Model at Mach Number 19
Author: Eugene C. Knox
Publisher:
Published: 1965
Total Pages: 0
ISBN-13:
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