Pressure and Heat-transfer Measurements on the Flat Face of a Blunted 10 Degree Half-cone Body (semidisk) at a Mach Number of 6.15 PDF Download

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Pressure and Heat-transfer Measurements on the Flat Face of a Blunted 10 Degree Half-cone Body (semidisk) at a Mach Number of 6.15

Pressure and Heat-transfer Measurements on the Flat Face of a Blunted 10 Degree Half-cone Body (semidisk) at a Mach Number of 6.15 PDF Author: P. Calvin Stainback
Publisher:
ISBN:
Category :
Languages : en
Pages : 21

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Book Description

Pressure and Heat-transfer Measurements on the Flat Face of a Blunted 10 Degree Half-cone Body (semidisk) at a Mach Number of 6.15

Pressure and Heat-transfer Measurements on the Flat Face of a Blunted 10 Degree Half-cone Body (semidisk) at a Mach Number of 6.15 PDF Author: P. Calvin Stainback
Publisher:
ISBN:
Category :
Languages : en
Pages : 21

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Book Description

Pressure and Heat-transfer Maesurements on the Flat Face of a Blunted 10° Half-cone Body (semidisk) at a Mach Number of 6.15

Pressure and Heat-transfer Maesurements on the Flat Face of a Blunted 10° Half-cone Body (semidisk) at a Mach Number of 6.15 PDF Author: P. Calvin Stainback
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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Book Description

Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 1196

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Book Description

Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on a Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90°

Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on a Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° PDF Author: Raul Jorge Conti
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 38

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Book Description
Two circulation conical configurations having 15° half-angles were tested in laminar boundary layer at a Mach number of 6 and angles of attack up to 90°. One cone had a sharp nose and a fineness ratio of 1.87 and the other had a spherically blunted nose with a bluntness ratio of 0.1428 and a fineness ratio of 1.66. Pressure measurements and schlieren pictures of the flow showed that near-conical flow existed above 70° high pressure areas were present near the base and the bow shock wave was considerably curved.

Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95

Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95 PDF Author: Jerome D. Julius
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 32

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Book Description

Laminar Heat-transfer Distributions for a Blunted-cone, Cone-frustum Reentry Configuration at Mach 10

Laminar Heat-transfer Distributions for a Blunted-cone, Cone-frustum Reentry Configuration at Mach 10 PDF Author: J. David Dearing
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 28

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Book Description

Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊

Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊ PDF Author: Dennis M. Bushnell
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 40

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Book Description

Experimental Investigation of the Pressures, Heat Transfer, and Surface Flow Patterns Around a Blunt Half-cone Lifting Reentry Body at a Mach Number of 9.6

Experimental Investigation of the Pressures, Heat Transfer, and Surface Flow Patterns Around a Blunt Half-cone Lifting Reentry Body at a Mach Number of 9.6 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 66

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Book Description

Heat-transfer and Pressure Measurements on Flat-face Cylinder at Mach Number Range of 2.49 to 4.44 [with List of References]

Heat-transfer and Pressure Measurements on Flat-face Cylinder at Mach Number Range of 2.49 to 4.44 [with List of References] PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

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Book Description

Exploratory Heat-transfer Measurements at Mach 10 on a 7.5 ̊total-angle Cone Downstream of a Region of Air and Helium Transpiration Cooling

Exploratory Heat-transfer Measurements at Mach 10 on a 7.5 ̊total-angle Cone Downstream of a Region of Air and Helium Transpiration Cooling PDF Author: James C. Dunavant
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 36

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Book Description
Heat transfer measurements at Mach 10 on total angle cone downstream of air and helium transpiration cooling region.