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Preliminary results from a free-flight investigation of boundary-layer transition and heat transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x 10⁶

Pressure Measurements on an Afterbody Behind Various Blunt Nose Shapes at a Mach Number of 2

Heat 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

Published Year

• 1950-1959 (3) *

Subject

• Boundary layer (1)
• Heat--Transmission (1)
• Thermal boundary layer (1)

Author

• Speegle, Katherine C. (3) *
• Chauvin, Leo T. (1)
• Hall, J. R. (1)
• Piland, Robert O. (1)

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