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Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44
Language: en
Pages: 26

Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44

Authors:
Categories:
Type: BOOK - Published: 1959 - Publisher:

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Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44
Language: en
Pages: 21

Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44

Authors: Stallings, Jr. (Robert L.)
Categories: Aerodynamic measurements
Type: BOOK - Published: 1959 - Publisher:

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Heat Transfer and Pressure Measurement on a 5-inch Hemispherical Concave Nose at a Mach Number of 2.0
Language: en
Pages: 24

Heat Transfer and Pressure Measurement on a 5-inch Hemispherical Concave Nose at a Mach Number of 2.0

Authors: J. Thomas Markley
Categories: Heat
Type: BOOK - Published: 1958 - Publisher:

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Abstract: The concave-nose stagnation-point heating is 40 percent of that of a hemisphere nose shape having the same diameter. At angles of attack of ℗±5© a
Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44
Language: en
Pages: 21

Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44

Authors: Stallings, Jr. (Robert L.)
Categories: Aerodynamic measurements
Type: BOOK - Published: 1959 - Publisher:

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Laminar Heat-transfer and Pressure-distribution Studies on a Series of Reentry Nose Shapes at a Mach Number of 19.4 in Helium
Language: en
Pages: 44

Laminar Heat-transfer and Pressure-distribution Studies on a Series of Reentry Nose Shapes at a Mach Number of 19.4 in Helium

Authors: Richard D. Wagner
Categories: Fluid mechanics
Type: BOOK - Published: 1961 - Publisher:

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